2013 Final Program - American Institute of Aeronautics and

Transcription

54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural
Dynamics, and Materials Conference
21st AIAA/ASME/AHS Adaptive Structures Conference
15th AIAA Non-Deterministic Approaches Conference
14th AIAA Dynamics Specialists Conference
8–11 April 2013
Boston Park Plaza
Hotel & Towers
Boston, Massachusetts
14th AIAA Gossamer Systems Forum
9th AIAA Multidisciplinary Design Optimization
Specialist Conference
FINAL PROGRAM
13-0130
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BENEFITS OF ATTENDANCE
WELCOME
The conference chairs and planning committee thank you for participating in the
co-located 54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics,
and Materials Conference, 21st AIAA/ASME/AHS Adaptive Structures
Conference, 15th AIAA Non-Deterministic Approaches Conference, 14th AIAA
Dynamics Specialists Conference, 14th AIAA Gossamer Systems Forum, and
9th AIAA Multidisciplinary Design Optimization Specialist Conference, held
8–11 April 2013 at the Boston Park Plaza Hotel & Towers in Boston, Massachusetts.
This event provides an unrivaled opportunity to gather the world’s leading
scientists, engineers, researchers, and managers from all over the world for technical
interchange and technology advancement. The co-location of these related AIAA
events provides attendees with a unique opportunity to expand their knowledge of
technological advances of these interrelated disciplines and explore areas of common
technical expertise.
This week you will:
• Present recent advances before a knowledgeable international audience
• Educate customers and providers on the latest research and product
developments
• Learn about the latest technology and research in the field from industry experts
• Network to engage new contacts and refresh old ones
• Recognize significant achievements from within the community
Here’s what to expect at this year’s event:
Program
• Keynote speakers on the Boeing 787, launch vehicles, space-based solar power,
genomics, uncertainty, game-changing technologies, and complex design
management
• Participation in more than 100 technical sessions covering all aspects of structures,
structural dynamics, materials, design engineering and optimization, survivability,
non-deterministic approaches, and gossamer spacecraft design, systems, and
operations
• Access to more than 550 technical papers and presentations
Networking Events
• Welcome Reception
• AIAA Awards Luncheon
• Networking Coffee Breaks
• Committee Meetings
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BENEFITS
ORGANIZING
OF ATTENDANCE
COMMITTEE
54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics,
and Materials Conference
General Chair
Anthony M. Waas
University of Michigan
Technical Program Chair
Ajit K. Roy
Air Force Research Laboratory
Student Papers Technical Chair
John D. Whitcomb
Texas A&M University
21st AIAA/ASME/AHS Adaptive Structures Conference
General Chair
David F. Voracek
NASA Dryden Flight Research Center
Ratneshwar (Ratan) Jha
Mississippi State University
15th AIAA Non-Deterministic Approaches Conference
General Chair
Gianluca Iaccarino
Stanford University
Ben Thacker
Southwest Research Institute
14th AIAA Dynamics Specialists Conference
General Chair
John B. Kosmatka
University of California, San Diego
Joseph C. Slater
Wright State University
14th AIAA Gossamer Systems Forum
General Chair
James D. Moore
ManTech Nexolve
Jeremy A. Banik
Air Force Research Laboratory
9th AIAA Multidisciplinary Design Optimization Specialist Conference
General Chair
Maxwell Blair
Bryn Athyn College
Andy Ko
Phoenix Integration
4
KEYNOTE SPEAKERS
Monday, 8 April 2013
Wednesday, 10 April 2013
0800–0900 hrs
0800–0900 hrs
Structures, Structural Dynamics,
and Materials (SDM) Conference
Opening Keynote
ASME Keynote
“Magnetostrictive Alloys: The Other Smart
Material”
Alison Flatau, Associate Dean for Research,
Clark School of Engineering, University of
Maryland, College Park, MD
“Beyond the 787: Developing the Future
of Structures and Materials that Shape
Aerospace”
John J. Tracy, Chief Technology Officer
and Senior Vice President, Engineering,
Operations, and Technology, The Boeing
Company, Chicago, IL
0800–0900 hrs
Dynamics Specialists Conference
(DSC) Keynote
“Launch Vehicle and Spacecraft Structural
Dynamics: State of the Art and Challenges
for the Future”
Alvar M. Kabe, Associate Principal Director,
Structural Mechanics Subdivision, The
Aerospace Corporation, El Segundo, CA
1300–1400 hrs
Structures, Structural Dynamics,
and Materials (SDM) Conference
Lecture
“Genomics of Multifunctional Structures
and Materials for Flight”
Dan Inman, Clarence “Kelly” Johnson
Professor and Chair, University of Michigan,
Ann Arbor, MI
1200–1400 hrs
AIAA Awards Luncheon
“Computational Models in the Materials
World: We Are Nearly There….”
David Furrer, Senior Fellow Discipline Lead,
Pratt & Whitney, East Hartford, CT (with
Rollie Dutton, Air Force Research Laboratory,
Wright-Patterson AFB, OH)
Tuesday, 9 April 2013
0800–0900 hrs
Non-Deterministic Approaches
(NDA) Conference Keynote
1800–1900 hrs
“Assuring Aero-Structural Reliability in an
Uncertain World”
Ravi Chona, USAF Senior Scientist and
Director, Structural Sciences Center, Air
Force Research Laboratory, Wright-Patterson
AFB, OH
Gossamer Systems Forum (GSF)
Keynote
“SPS-ALPHA: A Practical New Approach to
the Vision of the Solar Power Satellite”
John Mankins, CEO, Artemis Innovation
Management Solutions LLC, Santa Maria, CA
1300–1400 hrs
Thursday, 11 April 2013
Adaptive Structures Conference
(ASC) Keynote
“Game Changing Activities in the Area of
Lightweight Materials and Structures”
Stephen W. Gaddis, Program Manager, Org
A3 Game Changing Development Program
Office, NASA Langley Research Center,
Hampton, VA
0800–0900 hrs
Multidisciplinary Design
Optimization (MDO) Specialist
Conference Keynote
“The Role of the MDO in the Design for
Complex Engineered Systems”
Christina Bloebaum, Dennis and Rebecca
Muilenburg Professor for Aerospace
Engineering, Iowa State University, Ames, IA
5
BENEFITS
EVENT
AT OF
A GLANCE
ATTENDANCE
Saturday, 6 April 2013
Sunday, 7 April 2013
0700 hrs
Networking Coffee and Pastries
0730 hrs
Speakers’ Briefing in Session Rooms
0800 hrs
0830 hrs
SDM Opening
Keynote
0900 hrs
Networking Coffee Break
1000 hrs
Technical
Sessions
1030 hrs
1100 hrs
1130 hrs
1200 hrs
1230 hrs
Continuing
Education
Courses
Continuing
Education
Courses
Lunch Break
1300 hrs
SDM Lecture
1330 hrs
Registration Open
0930 hrs
Networking Coffee Break /
1400 hrs
1430 hrs
Registration Open
1500 hrs
1530 hrs
1600 hrs
1630 hrs
1700 hrs
1730 hrs
1800 hrs
Technical
Sessions
Welcome Reception
1830 hrs
1900 hrs
1930 hrs
2000 hrs
2030 hrs
Committee Meetings
Committee Meetings
2100 hrs
2130 hrs
NETWORKING ACTIVITIES AND SPECIAL EVENTS
Networking Coffee Breaks
A great way to start the day and interact with conference
participants! Coffee and pastries will be offered on Monday–
Thursday, 0700–0800 hrs, in the Plaza Ballroom at the Boston
Park Plaza Hotel & Towers. This event is open to all attendees
(no tickets required).
Stand-alone networking coffee breaks are included in the
program to allow even more time for making new contacts,
continuing discussions from technical sessions, or checking
emails and voicemails to keep in touch with the office while
you are at the conference. Networking coffee breaks will be
located in the Plaza Ballroom at the Boston Park Plaza Hotel &
Towers at the following times:
0900–0930 hrs and 1400–1430 hrs
0900–0930 hrs and 1400–1430 hrs
Wednesday, 10 April 2013 0900–0930 hrs and 1400–1430 hrs
Thursday, 11 April 2013 0900–0930 hrs
6
EVENT AT A GLANCE
0700 hrs
0730 hrs
0800 hrs
NDA Keynote
ASME Keynote /
DSC Keynote
MDO Keynote
Technical
Sessions
Technical
Sessions
Technical
Sessions
0830 hrs
0900 hrs
1100 hrs
1130 hrs
1200 hrs
1230 hrs
1300 hrs
1330 hrs
1400 hrs
Lunch Break
ASC Keynote
Awards Luncheon
Technical
Sessions
Technical
Sessions
1430 hrs
1500 hrs
1530 hrs
1600 hrs
1630 hrs
Lunch Break
Registration Open
1030 hrs
Registration Open
1000 hrs
Registration Open
0930 hrs
Technical
Sessions
1700 hrs
1730 hrs
1800 hrs
GSF Keynote
1830 hrs
1900 hrs
1930 hrs
2000 hrs
2030 hrs
Committee Meetings
Committee Meetings
2100 hrs
2130 hrs
NETWORKING ACTIVITIES AND SPECIAL EVENTS
Welcome Reception
A welcome reception will be held on Monday, 8 April 2013,
1800–1930 hrs, in the Georgian Ballroom at the Boston Park
Plaza Hotel & Towers. Take this opportunity to engage new
contacts and refresh old ones. A ticket for the reception is
required and included in the conference registration fee where
indicated. Additional tickets for guests may be purchased upon
registration or on site, as space is available.
Join fellow conference participants to recognize the
achievements of your peers at the AIAA Awards Luncheon
on Wednesday, 10 April 2013, 1200–1400 hrs, in the Imperial
Ballroom at the Boston Park Plaza Hotel & Towers. Several
awards will be presented, as well as a keynote speech by
David Furrer, Senior Fellow Discipline Lead, Pratt &
Whitney, East Hartford, CT (with Rollie Dutton, Air Force
Research Laboratory, Wright-Patterson AFB, OH). A ticket
for the luncheon is required and included in the conference
registration fee where indicated. Additional tickets for guests
may be purchased upon registration or on site, as space is
available.
7
BENEFITSPRESENTATION
AWARDS
OF ATTENDANCE
The following awards will be presented during this year’s AIAA
Awards Luncheon:
ASME/Boeing Best Paper
AIAA-ASC James H. Starnes, Jr.
Awards
Robert T. Britt, Daniel Ortega, Boeing Research &
Technology; John McTigue, Boeing Defense, Space & Security;
and Matthew J. Scott, NextGen Aeronautics Inc.
AIAA 2012-1464, “Wind Tunnel Test of a Very Flexible
Aircraft Wing”
Michael W. Hyer
N. Waldo Harrison Professor Emeritus
Department of Engineering Science and
Mechanics
Virginia Polytechnic Institute and State
University
Blacksburg, VA
Collier Research HyperSizer/
AIAA Structures Best Paper
Rauno Cavallaro, Luciano Demasi, and Andrea Passariello
San Diego State University
“ For a distinguished career advancing
composite structures, serving and
promoting the profession, and nurturing
the next generation of researchers.”
AIAA 2012-1462, “Nonlinear Analysis of PrandtlPlane
Joined Wings—Part II: Effects of Anisotropy”
AIAA Gossamer Systems Forum
Best Paper
Keith T. Kedward
Professor, Department of Mechanical
Engineering
University of California, Santa Barbara
Santa Barbara, CA
Daniel Vernon Guerrant and Dale A. Lawrence
University of Colorado-Boulder
William Keats Wilkie, NASA Langley Research Center
“ For his lifelong contributions in the field
of composite structural mechanics and his
devotion to the mentoring of students and
colleagues.”
AIAA 2012-1746, “Heliogyro Blade Twist Control via
Reflectivity Modulation”
AIAA Ashley Award for Aeroelasticity
In addition, recipients of the following awards
will be announced:
Dewey Hodges
Professor, School of Aerospace Engineering
Georgia Institute of Technology
Atlanta, GA
Jefferson Goblet Student Paper Award
The Harry H. and Lois G. Hilton Student Paper
Award in Structures
“ For lasting contributions to analysis
methodology for aeroelasticity of rotorcraft
and high-aspect-ratio wings, and
development of educational materials for
undergraduate study of aeroelasticity.”
Lockheed Martin Student Paper Award in
Structures
American Society for Composites Student Paper
in Composites Award
8
SPEAKERS AND SESSION CHAIRS
NEW! Speakers’ Briefings in Session Rooms
Session Chair Reports
Authors who are presenting papers, session chairs, and cochairs will meet for a short briefing in their session rooms
on the day of their sessions to exchange bios and review
final details prior to the session. Morning sessions will meet
0730–0800 hrs and afternoon sessions will meet 30 minutes
prior to the start of the session. Please attend on the day of
your session(s). Laptops pre-loaded with the Speakers’ Briefing
preparation slides will be provided in each session room. The
Speakers’ Briefing schedule is as follows:
All session chairs are asked to complete a session chair
report to evaluate their session for future planning. AIAA
has partnered with Canvas Solutions to provide an electronic
Session Chair Report form. You can download the FREE
mobile app in your App Store, AppWorld, or Marketplace by
searching for “Canvas Solutions, Inc.” The mobile app is free,
so please make sure to download it. Detailed instructions will
be provided in the session rooms. If you do not have a tablet or
a smartphone, simply use this form as a guide and enter your
session chair report information at the session chair reporting
computer station located on site near the AIAA registration
area. Report data is collected and used for future planning
purposes, including session topics and room allocations. Please
submit your session chair report electronically by 12 April
2013.
Morning Sessions
Afternoon Sessions
0730–0800 hrs
1400–1430 hrs
Morning Sessions
Afternoon Sessions
Audiovisual
0730–0800 hrs
1400–1430 hrs
Each session room will be preset with the following: one LCD
projector, one screen, one microphone and sound system (if
necessitated by room size), and one laser pointer. This year,
laptop computers will also be provided. You may also use
your own computer. Any additional audiovisual equipment
requested on site will be at cost to the presenter. Please note
that AIAA does not provide security in the session rooms and
recommends that items of value not be left unattended.
Morning Sessions
Afternoon Sessions
0730–0800 hrs
1400–1430 hrs
Morning Sessions
Afternoon Sessions
0730–0800 hrs
1300–1330 hrs
Timing of Presentations
Speakers’ Practice Room
Each paper presentation is allotted 30 minutes (included
introduction and question-and-answer period), except where
noted.
Speakers who wish to practice their presentations may do so
in the Board Room (on the 4th floor) at the Boston Park Plaza
Hotel & Towers. A sign-up sheet will be posted on the door. In
consideration of others, please limit practice time to 30-minute
increments.
“No Paper, No Podium” Policy
This conference has a “No Paper, No Podium” policy. If
a written paper is not submitted by the final manuscript
deadline, authors will not be permitted to present the paper at
the conference. This policy is intended to improve the quality
of the program for the attendees.
9
BENEFITS INFORMATION
GENERAL
OF ATTENDANCE
AIAA Registration and Information
Center Hours
Cyber Café
The AIAA Registration and Information Center will be located
outside the Exeter room at the Boston Park Plaza Hotel &
Towers. Hours are as follows:
Computers with complimentary Internet access for conference
attendees will be available at the AIAA Cyber Café, located in
the foyer on the 2nd floor at the Boston Park Plaza Hotel &
Towers. Hours of operation are as follows:
1500–1900 hrs
0700–1700 hrs
0700–1700 hrs
0700–1700 hrs
0700–1700 hrs
1500–1900 hrs
0700–1700 hrs
0700–1700 hrs
0700–1700 hrs
0700–1700 hrs
Wi-Fi Internet Access On Site: AIAA may provide limited
Wi-Fi service for attendees to use while on site. To keep this
service available and optimized for all attendees, please do not
download files larger than 2MB, create multiple sessions across
multiple devices, or download multiple files in one session. If
you receive an error message that an AIAA server is blocking
your current IP address, please inform the AIAA registration
desk.
Meeting Site
Boston can perhaps be best described as a welcome
contradiction: Hip alongside historic. Skyscrapers surround
parks. Gourmet meets pizza. There’s history and culture around
every bend in Boston—skyscrapers nestle next to historic
hotels while modern marketplaces line the antique cobblestone
streets. When visiting Boston, you’ll discover neighborhoods
with distinct character, quaint brownstone-lined streets,
Boston’s beloved Red Sox, and big-city entertainment. For more
information, visit www.bostonusa.com.
30% Off All Books at SDM and Co-Located
Conferences
AIAA Publications is offering a special show discount on
all titles featured at the SDM and Co-located Conferences.
Attendees can take advantage of a 30% discount off the list
price of all books for sale at the AIAA Bookstore. This show
special will only be available during the conference! Also
featured will be the entire 2013 AIAA Book of the Month
collection at their special month prices. Lastly, Finite Element
Structural Analysis: New Concepts, by J.S. Przemieniecki,
has been selected as the conference book for this year’s SDM
conference, and is on sale for $58.47. Take advantage of these
super savings and visit the AIAA Bookstore!
Conference Proceedings
Proceedings for these conferences will be available in online
proceedings format. The cost is included in the registration
fee where indicated. The online proceedings will be available
on 8 April 2013. Attendees who register in advance for the
online proceedings will be provided with instructions on how
to access them. Those registering on site will be provided with
instructions at that time.
Journal Publication
Authors of appropriate papers are encouraged to submit
them for possible publication in one of the Institute’s archival
journals: AIAA Journal; Journal of Aircraft; Journal of Guidance,
Control, and Dynamics; Journal of Propulsion and Power;
Journal of Spacecraft and Rockets; Journal of Thermophysics
and Heat Transfer; or Journal of Aerospace Information Systems
(formerly Journal of Aerospace Computing, Information, and
Communication). You may now submit your paper online at
http://mc.manuscriptcentral.com/aiaa.
10
GENERAL INFORMATION
Certificate of Attendance
Professional Committee, is available to help you gain support
and financial backing from your company. The guide explains
the benefits of participation, offers recommendations and
provides an example letter for seeking management support
and funding, and shows you how to get the most out of your
participation. The online guide can be found on the AIAA
website at www.aiaa.org/YPGuide.
Certificates of Attendance are available for attendees who
request documentation at the conference itself. Please
request your copy at the on-site registration desk. AIAA
offers this service to better serve the needs of the professional
community. Claims of hours or applicability toward
professional education requirements are the responsibility of
the participant.
Membership
Messages and Information
Nonmembers who pay the full nonmember registration fee will
receive their first year’s AIAA membership at no additional cost.
Messages will be recorded and posted on a bulletin board in
the registration area. It is not possible to page attendees.
Nondiscriminatory Practices
Employment Opportunities
AIAA accepts registrations irrespective of race, creed, sex,
color, physical handicap, and national or ethnic origin.
AIAA assists members who are searching for employment
by providing a bulletin board at technical meetings. This
bulletin board is solely for “open position” and “available for
employment” postings. Employers are encouraged to have
personnel who are attending an AIAA technical conference
bring “open position” job postings. Individual AIAA members
may post “available for employment” notices. AIAA cannot
assume responsibility for notices forwarded to AIAA
Headquarters. AIAA reserves the right to remove inappropriate
notices. AIAA members can post and browse resumes, browse
job listings, and access other online employment resources by
visiting the AIAA Career Center at http://careercenter.aiaa.org.
Restrictions
Video or audio recording of sessions or technical exhibits, as
well as the unauthorized sale of AIAA-copyrighted material, is
prohibited.
International Traffic in Arms Regulations
(ITAR)
AIAA speakers and attendees are reminded that some
topics discussed in the conference could be controlled
by the International Traffic in Arms Regulations (ITAR).
U.S. nationals (U.S. citizens and permanent residents) are
responsible for ensuring that technical data they present
in open sessions to non-U.S. nationals in attendance or in
conference proceedings are not export restricted by the ITAR.
U.S. nationals are likewise responsible for ensuring that they do
not discuss ITAR export-restricted information with non-U.S.
nationals in attendance.
Young Professional Guide for Gaining
Management Support
Young professionals have the unique opportunity to meet and
learn from some of the most important people in the business
by attending conferences and participating in AIAA activities.
A detailed online guide, published by the AIAA Young
AIAA is the world’s largest technical society dedicated to
the global aerospace profession. With more than 35,000
individual members worldwide, and 100 corporate members,
AIAA brings together industry, academia, and government
to advance engineering and science in aviation, space, and
defense.
American Institute of Aeronautics and Astronautics
1801 Alexander Bell Drive, Suite 500
Reston, VA 20191-4344
703.264.7500 or 800.639.AIAA (2422)
Fax: 703.264.7657
custserv@aiaa.org
www.aiaa.org
11
BENEFITS OFMEETINGS
COMMITTEE
ATTENDANCE
Time
Committee
Location
1830–2200 hrs
Structures TC
Whittier
1930–2100 hrs
SciTech 2014 SDM Technical Program Committee Meeting
White Hill
1130–1330 hrs
Aerospace Design and Structures Group
Terrace
1900–2200 hrs
DETC Subcommittee Meeting
Stuart
1900–2200 hrs
Survivability TC
Clarendon
1900–2200 hrs
Multidiciplinary Design Optimization TC
Whittier
1930–2130 hrs
ASME Structures and Materials Technical Committee
Lexington
1200–1330 hrs
SDM Long Range Planning Committee Meeting
Terrace
1900–2200 hrs
Materials TC
White Hill
1900–2200 hrs
Structures TC
Terrace
1900–2200 hrs
Design Engineering TC
Clarendon
1900–2200 hrs
Adaptive Structures TC
Arlington/Berkley
1900–2200 hrs
Structural Dynamics TC
Georgian
1900–2200 hrs
Non-Deterministic Approaches TC
Whittier
1930–2200 hrs
Gossamer Spacecraft PC
Whittier
12
BENEFITS OF
PROGRAM
ATATTENDANCE
A GLANCE
Session No.
Session Title
Start Time
Location
0700 hrs
Plaza Ballroom
1-NB-1
Monday Networking Coffee and Pastries
2-SB-1
Monday Morning Speakers’ Briefing
0730 hrs
Session Rooms
3-PLNRY-1
Structures, Structural Dynamics, and Materials (SDM) Conference
Opening Keynote
0800 hrs
Imperial Ballroom
4-BRK-1
Monday Morning Networking Coffee Break
0900 hrs
Plaza Ballroom
5-ASC-1
Morphing Structures I
0930 hrs
Statler
6-DSC-1
Hypersonics I
0930 hrs
Lexington
7-GSF-1
Special Session: Testing of Lightweight Space Structures
0930 hrs
Thoreau
8-MDO-1
Optimization Applications I
0930 hrs
Cabot
9-NDA-1
Non-Deterministic Methods I
0930 hrs
Winthrop
10-SDM-1
Analytical Methods for Structures I
0930 hrs
Constitution
11-SDM-2
Fatigue and Fracture
0930 hrs
St. James
12-SDM-3
Structural Optimization
0930 hrs
Stuart
13-SDM-4
Air and Space Survivability
0930 hrs
Berkley
14-SDM-5
Aeroservoelasticity and Control
0930 hrs
Beacon Hill
15-SDM-6
Aircraft Gust I
0930 hrs
White Hill
16-SDM-7
Structural Health Monitoring I
0930 hrs
Cambridge
17-SDM-8
Characterization and Estimation of Fatigue Life I
0930 hrs
Charles River
18-SDM-9
Design Process
0930 hrs
Clarendon
19-SDM-10
Nonlinear and Nonlocal Material Response
0930 hrs
Imperial Ballroom
20-LNCH-1
Monday Lunch Break
1200 hrs
21-SDM-11
SDM Lecture
1300 hrs
22-BRK-2
Monday Afternoon Networking Coffee Break
1400 hrs
Plaza Ballroom
23-SB-2
Monday Afternoon Speakers’ Briefing
1400 hrs
Session Rooms
24-ASC-2
Morphing Structures II
1430 hrs
Statler
25-DSC-2
Multidisciplinary Analysis for Combined Environment Structures I
1430 hrs
Lexington
26-GSF-2
Large Area Space Structures
1430 hrs
Thoreau
27-MDO-2
Aero-Structural Optimization
1430 hrs
Cabot
28-MDO-3
Optimization Frameworks and Applications
1430 hrs
Constitution
29-NDA-2
Non-Deterministic Methods II
1430 hrs
Winthrop
30-SDM-12
Composites: Analytical Methods I
1430 hrs
St. James
Imperial Ballroom
KEY
ASC
Adaptive Structures Conference (ASC)
ASME
ASME Keynote
BRK
DSC
Dynamic Specialist Conference (DSC)
GSF
Gossamer Systems Forum (GSF)
LNCH
Lunch Break
MDO
Multidisciplinary Design Optimization
(MDO) Conference
13
NB
NDA
Non-Deterministic Approaches (NDA)
Conference
PLNRY
Plenary Session
RCPT
Welcome Reception
SB
SDM
Structures, Structural Dynamics, and
Materials (SDM) Conference
PROGRAM AT A GLANCE
Session No.
Session Title
Start Time
Location
31-SDM-13
Sandwich Structures
1430 hrs
Stuart
32-SDM-14
Wind Turbine Dynamics, Loads, and Control
1430 hrs
Berkley
33-SDM-15
Aircraft Design and Nonlinear Dynamics
1430 hrs
Beacon Hill
34-SDM-16
Beam Dynamics I
1430 hrs
White Hill
35-SDM-17
Energy Harvesting and Aeroservoelasticity Design
1430 hrs
Cambridge
36-SDM-18
Design: Spacecraft I
1430 hrs
Charles River
37-SDM-19
Digital Twin I
1430 hrs
Clarendon
38-SDM-20
Nanostructured Materials I
1430 hrs
Imperial Ballroom
39-SDM-21
Additive Manufacturing
1430 hrs
Franklin
40-RCPT-1
Welcome Reception
1800 hrs
Georgian Ballroom
41-NB-2
Tuesday Networking Coffeee and Pastries
0700 hrs
Plaza Ballroom
42-SB-3
Tuesday Morning Speakers’ Briefing
0730 hrs
Session Rooms
43-NDA-3
Non-Deterministic Approaches (NDA) Conference Keynote
0800 hrs
Imperial Ballroom
44-BRK-3
Tuesday Morning Networking Coffee Break
0900 hrs
Plaza Ballroom
45-ASC-3
Space Applications
0930 hrs
Statler
46-DSC-3
Hypersonics II
0930 hrs
Lexington
47-GSF-3
Membrane Packaging and Applications
0930 hrs
Thoreau
48-MDO-4
Optimization Applications II
0930 hrs
Cabot
49-NDA-4
Non-Deterministic Fatigue and Fracture
0930 hrs
Winthrop
50-SDM-22
Analytical Methods for Structures II
0930 hrs
Constitution
51-SDM-23
Composites: Fatigue and Fracture I
0930 hrs
St. James
52-SDM-24
Composites: Impact, Damage, and Voids
0930 hrs
Stuart
53-SDM-25
Structural Health Monitoring II
0930 hrs
Franklin
54-SDM-26
Wind Turbine Blade Composite Material Analysis and Testing
0930 hrs
Berkley
55-SDM-27
Aircraft Dynamics
0930 hrs
White Hill
56-SDM-28
Aircraft Gust II
0930 hrs
Cambridge
57-SDM-29
Beam Dynamics II
0930 hrs
Beacon Hill
58-SDM-30
MAVs and Flapping Wings I
0930 hrs
Imperial Ballroom
59-SDM-31
Characterization and Estimation of Fatigue Life II
0930 hrs
Charles River
60-SDM-32
Digital Twin II and Multiscale Modeling of Damage in Composites I
0930 hrs
Clarendon
61-LNCH-2
Tuesday Lunch Break
1200 hrs
62-ASC-4
Adaptive Structures Conference (ASC) Keynote
1300 hrs
63-BRK-4
Tuesday Afternoon Networking Coffee Break
1400 hrs
Plaza Ballroom
64-SB-4
Tuesday Afternoon Speakers’ Briefing
1400 hrs
Session Rooms
65-ASC-5
Structural Health Monitoring III
1430 hrs
Statler
66-DSC-4
Multidisciplinary Analysis for Combined Environment Structures II
1430 hrs
Lexington
67-GSF-4
Flexible Composites: Hinges and Booms
1430 hrs
Thoreau
68-MDO-5
Aerodynamic and Aircraft Optimization
1430 hrs
Cabot
69-NDA-5
Non-Deterministic Methods for Aerospace Applications
1430 hrs
Winthrop
70-SDM-33
Composite Structures
1430 hrs
St. James
14
Imperial Ballroom
PROGRAM AT A GLANCE
Session No.
Session Title
Start Time
Location
71-SDM-34
Structural Design I
1430 hrs
Cambridge
72-SDM-35
Wind Turbine Structural Dynamics and Aeroelasticity
1430 hrs
Berkley
73-SDM-36
Computational Aeroservoelasticity
1430 hrs
Beacon Hill
74-SDM-37
MAVs and Flapping Wings II
1430 hrs
Clarendon
75-SDM-38
Rotorcraft Applications
1430 hrs
White Hill
76-SDM-39
Design: Advanced Aircraft
1430 hrs
Charles River
77-SDM-40
Multiscale Modeling of Damage in Composites II
1430 hrs
Stuart
78-SDM-41
Nanostructured Materials II
1430 hrs
Imperial Ballroom
80-SDM-43
Stitched Unitized Structures
1430 hrs
Constitution
81-NB-3
Wednesday Networking Coffee and Pastries
0700 hrs
Plaza Ballroom
82-SB-5
Wednesday Morning Speakers’ Briefing
0730 hrs
Session Rooms
83-ASME-1
ASME Keynote
0800 hrs
Georgian Ballroom
84-DSC-5
Dynamic Specialist Conference (DSC) Keynote
0800 hrs
Imperial Ballroom
85-BRK-5
Wednesday Morning Networking Coffee Break
0900 hrs
Plaza Ballroom
86-ASC-6
Active Control of Structures
0930 hrs
Statler
87-DSC-6
Multidisciplinary Analysis for Combined Environment Structures III
0930 hrs
Lexington
88-MDO-6
Optimization Methods
0930 hrs
Cabot
89-NDA-6
Optimization Under Uncertainty I
0930 hrs
Winthrop
90-SDM-44
Composites: Analytical Methods II
0930 hrs
St. James
91-SDM-45
Composites: Damage Evolution
0930 hrs
Cambridge
92-SDM-46
Shells
0930 hrs
Charles River
93-SDM-47
Turbomachinery
0930 hrs
Clarendon
94-SDM-48
Vibration Testing I
0930 hrs
Beacon Hill
95-SDM-49
Characterization and Modeling of Composite Laminates
0930 hrs
Berkley
96-SDM-50
Design: Micro/Unmanned Aircraft
0930 hrs
Constitution
97-SDM-51
Multifunctional Materials I
0930 hrs
Stuart
98-SDM-52
Integrated Computational Material Engineering and the Materials
Genome Initiative
0930 hrs
Franklin
99-LNCH-3
1200 hrs
Imperial Ballroom
100-BRK-6
Wednesday Afternoon Networking Coffee Break
1400 hrs
Plaza Ballroom
101-SB-6
Wednesday Afternoon Speakers’ Briefing
1400 hrs
Session Rooms
102-ASC-7
Modeling and Analysis I
1430 hrs
Franklin
103-DSC-7
The Aeroelastic Prediction Workshop
1430 hrs
Lexington
104-GSF-6
Solar Sails and Drag De-Orbiters
1430 hrs
Thoreau
105-MDO-7
Composite and Structural Optimization I
1430 hrs
Cabot
106-NDA-7
Optimization Under Uncertainty II
1430 hrs
Winthrop
107-NDA-8
Reliability Testing
1430 hrs
St. James
108-SDM-53
Joints, Aeroelasticity, and Buckling
1430 hrs
Cambridge
109-SDM-54
Space Structures
1430 hrs
Clarendon
110-SDM-55
Damping and Vibration Suppression
1430 hrs
Beacon Hill
111-SDM-56
Limit Cycle Oscillations (LCO) and Aircraft Flutter
1430 hrs
Berkley
15
PROGRAM AT A GLANCE
Session No.
Session Title
Start Time
Location
112-SDM-57
Design: Spacecraft II
1430 hrs
Charles River
113-SDM-58
Integrated Computational Materials Engineering (ICME)
1430 hrs
Stuart
114-SDM-59
Nanostructured Materials III
1430 hrs
Constitution
115-GSF-7
Gossamer Systems Forum (GSF) Keynote
1800 hrs
Georgian Ballroom
116-NB-4
Thursday Networking Coffee and Pastries
0700 hrs
Plaza Ballroom
117-SB-7
Thursday Morning Speakers’ Briefing
0730 hrs
Session Rooms
118-MDO-8
Multidisciplinary Design Optimization (MDO) Conference Keynote
0800 hrs
Imperial Ballroom
119-BRK-7
Thursday Morning Networking Coffee Break
0900 hrs
Plaza Ballroom
120-DSC-8
Computational Aeroelasticity I
0930 hrs
Franklin
121-GSF-8
Inflatable Structures
0930 hrs
Thoreau
122-MDO-9
Topology Optimization
0930 hrs
Cabot
123-NDA-9
Non-Deterministic Model Validation and Calibration
0930 hrs
Winthrop
124-SDM-60
Composites: Fatigue and Fracture II
0930 hrs
Lexington
125-SDM-61
Structural Design II
0930 hrs
Cambridge
126-SDM-62
Space and Launch Vehicle Structural Dynamics
0930 hrs
Beacon Hill
127-SDM-63
String, Cable, and Wiring Dynamics
0930 hrs
Clarendon
128-SDM-64
Very Flexible Aircraft
0930 hrs
St. James
129-SDM-65
Vibration Testing II
0930 hrs
Berkley
130-SDM-66
Multifunctional Materials II and Materials for Structural Health
Monitoring
0930 hrs
Stuart
131-SDM-67
Processes in Aerospace Materials
0930 hrs
Statler
132-LNCH-4
Thursday Lunch Break
1200 hrs
133-SB-8
Thursday Afternoon Speakers’ Briefing
1300 hrs
Session Rooms
134-ASC-8
Modeling and Analysis II
1330 hrs
Statler
135-ASC-9
SMA Applications
1330 hrs
Cambridge
136-DSC-9
Computational Aeroelasticity II
1330 hrs
Franklin
137-GSF-9
Membrane Mechanics and Active Control
1330 hrs
Thoreau
138-MDO-10
Composite and Structural Optimization II
1330 hrs
Cabot
139-NDA-10
Non-Deterministic Model Error and Selection
1330 hrs
Clarendon
140-NDA-11
Non-Deterministic Maintenance, Monitoring and Prognostics
1330 hrs
Winthrop
141-SDM-68/
GSF-10
Membrane Structural Dynamics
1330 hrs
Beacon Hill
142-SDM-69
Plate and Cylinder Dynamics
1330 hrs
Berkley
143-SDM-70
Multiscale Modeling and Characterization of Composites
1330 hrs
Stuart
16
17
Monday Morning Speakers’ Briefing
2-SB-1
0730 - 0800 hrs
Technical University of Lisbon, Lisbon,
Portugal
W. Mallik, R. Kapania, J. Schetz, Virginia
Polytechnic Institute and State University,
Blacksburg, VA
J. Gariffo, O. Bendiksen, University of
California, Los Angeles, Los Angeles, CA
Research Laboratory, Wright-Patterson
AFB, OH
Chaired by: W. WELSH, Sikorsky Aircraft Corporation and A. SCOTTI, Pilatus Aircraft Ltd
0930 hrs
1000 hrs
1030 hrs
AIAA-2013-1455
AIAA-2013-1456
AIAA-2013-1454
Efficient Prediction of Transonic
Equivalent Structural Models for
Optimization of Medium-Range
Flutter Boundaries with Linearized Aeroelastic Design of High-Speed
Transonic Truss-Braced Wing
Aeroservoelastic Reduced-Order
Flight Vehicles
M. Bhatia, P. Beran, B. Stanford, Air Force
Aircraft with Flutter Constraint
Models
6-DSC-1
J. Cardoso, A. Suleman, Technical University of Swansea University, Swansea, United
Lisbon, Lisbon, Portugal; J. Cooper, University Kingdom
of Bristol, Bristol, United Kingdom
B. Zuchowski, Lockheed Martin
Corporation, Palmdale, CA
1100 hrs
AIAA-2013-1457
Structural Response and Service
Life Prediction Concerns in the
Design of Hypersonic Flight Vehicle
Hot-Structure
Hypersonics I
J. Vale, F. Lau, Technical University of
Lisbon, Lisbon, Portugal; A. Suleman,
University of Victoria, Victoria, Canada
1100 hrs
AIAA-2013-1453
Optimal Control and Energy
Balance Evaluation of a Morphing
Aircraft
Morphing Structures I
Monday Morning Networking Coffee Break
Beyond the 787: Developing the Future of Structures and Materials that Shape Aerospace
John J. Tracy
Chief Technology Officer and Senior Vice President, Engineering, Operations, and Technology, The Boeing Company, Chicago, IL
Structures, Structural Dynamics, and Materials (SDM) Conference Opening Keynote
Chaired by: D. MCGOWAN, NASA Langley Research Center and E. WHITE, The Boeing Company
1000 hrs
1030 hrs
0930 hrs
AIAA-2013-1450
AIAA-2013-1451
AIAA-2013-1452
Variable Wing Span Using the
Study of an Articulated Winglet
Performance Evaluation of a
Compliant Spar Concept
Mechanism
Morphing Joined Wing Aircraft
R. Ajaj, E. Saavedra Flores, M. Friswell,
A. Gomes, L. Falcao, A. Suleman,
Configuration
5-ASC-1
4-BRK-1
0900 - 0930 hrs
3-PLNRY-1
0800 - 0900 hrs
Session Chairs and Speakers for Monday morning sessions will meet in their assigned session room.
Monday Networking Coffee and Pastries
1-NB-1
0700 - 0800 hrs
Monday
Lexington
Statler
Plaza Ballroom
Imperial Ballroom
In Session Rooms
Plaza Ballroom
18
Ottawa, Canada
M. Islam, R. Kapania, Virginia Polytechnic
Institute and State University, Blacksburg, VA
1100 hrs
AIAA-2013-1475
A Damage Tolerance Study of
Curvilinearly Stiffened Panels with
Different Crack Lengths Using a
Global-local Finite Element Method
E. Pineda, B. Bednarcyk, S. Arnold, NASA
Glenn Research Center, Cleveland, OH
Analytical Methods for Structures I
1130 hrs
AIAA-2013-1471
An New Technique in Analytical
Reliability Estimation Involving Multimodal Distributions: An Extended
Laplace Approximation Approach
K. Shimoyama, Tohoku University, Sendai,
Japan; S. Kawai, Japan Aerospace Exploration X. Guan, J. Zhang, S. Zhou, Siemens
Agency (JAXA), Sagamihara, Japan; J. Alonso, Corporation, Princeton, NJ; R. Jha,
Stanford University, Stanford, CA
Mississippi State University, Starkville, MS
1100 hrs
AIAA-2013-1470
Dynamic Adaptive Sampling Based
on Kriging Surrogate Models for
Efficient Uncertainty Quantification
J. Deaton, R. Grandhi, Wright State
University, Dayton, OH
1130 hrs
AIAA-2013-1466
Topology Optimization of Thermal
Structures with Stress Constraints
Chaired by: B. WARDLE, Massachusettes Institute of Technology and M. CHO, Seoul National University
1000 hrs
1030 hrs
0930 hrs
AIAA-2013-1473
AIAA-2013-1474
AIAA-2013-1472
Representative Structural Element: A Study of the Adhesive Joints and On Multiscale Modeling: Preserving
Crack Propagation Using a Global- Energy Dissipation across the
a New Paradigm for Multiscale
local Finite Element Method
Scales with Consistent Handshaking
Structural Modeling
W. Yu, Utah State University, Logan, UT
M. Islam, R. Kapania, Virginia Polytechnic
Methods
W. Verhaeghe, W. Desmet, D. Vandepitte,
Catholic University of Leuven, Leuven,
Belgium; D. Moens, Lessius University
College, Sint-Katelijne-Waver, Belgium
1030 hrs
AIAA-2013-1469
Interval Field Implementations for
Spatial Uncertainty Processing in
Non-Deterministic FE Analysis
Non-Deterministic Methods I
1100 hrs
AIAA-2013-1465
Aircraft Tolerance Optimization
Considering Quality, Manufacturing
& Performance
K. Bhachu, G. Waycaster, R. Haftka, N.
N. Zafar, Beihang University, Beijing, China Kim, University of Florida, Gainesville,
Gainesville, FL
1030 hrs
AIAA-2013-1464
A Multiobjective, Multidisciplinary
Design Optimization of Solid
Propellant Based Space Launch
Vehicle
Optimization Applications I
10-SDM-1
W. Subber, A. Sarkar, Carleton University,
Ottawa, Canada
Chaired by: B. BICHON, Southwest Research Institue
0930 hrs
1000 hrs
AIAA-2013-1467
AIAA-2013-1468
Two-Level Domain Decomposition Data Assimilation for Large-Scale
Method for Uncertainty
Computational Models
M. Khalil, A. Sarkar, Carleton University,
Quantification
9-NDA-1
J. Allison, D. Herber, University of Illinois,
Urbana-Champaign, Urbana, IL
Chaired by: R. KAPANIA and R. GRANDHI, Wright State University
0930 hrs
1000 hrs
AIAA-2013-1462
AIAA-2013-1463
Multidisciplinary Optimization of
Optimization of Dynamic
Microwave Antennas
B. Duan, Xidian University, Xi’an, China
Engineering Systems
8-MDO-1
Kirtland AFB, NM; M. Peterson, University D. Di Maio, University of Bristol, Bristol,
of New Mexico, Albuquerque, NM
United Kingdom
P. Tarazaga, Virginia Polytechnic Institute
and State University, Blacksburg, VA; N.
Ameri, University of Bristol, Bristol, United
Kingdom
1100 hrs
AIAA-2013-1461
Non-contact point excitation
of ultra lightweight structures:
membranes
Special Session: Testing of Lightweight Space Structures
Chaired by: C. JENKINS, Montana State University and P. TARAZAGA, Virginia Tech
0930 hrs
1000 hrs
1030 hrs
AIAA-2013-1458
AIAA-2013-1459
AIAA-2013-1460
MOIRE Space Telescope-Challenges Design and Testing of Self-Deploying Simulation and measurement of inplane vibrations of an ultra lightweight
and Solutions in Large Scale Testing Membrane Optic Support Structure
W. Tandy, P. Atcheson, J. Domber, J.
Using Rollable Composite Tape Springs membrane using a newly designed
Kommers, Ball Aerospace & Technologies J. Footdale, LoadPath, Albuquerque, NM; 6DOF laser scanning head performing
Corporation, Boulder, CO
T. Murphey, Air Force Research Laboratory, conical scan measurements
7-GSF-1
Constitution
Winthrop
Cabot
Thoreau
19
B. Sayar, A. Kayran, Middle East Technical
University, Ankara, Turkey
Lockheed Martin Corporation, Palo Alto, CA;
C. Rankin, Rhombus Consultants Group, Palo
Alto, CA
Z. Wu, G. Raju, P. Weaver, University of
Bristol, Bristol, United Kingdom
Texas, Austin, Austin, TX
Aeronautics (ITA), São José dos Campos, Y. Yang, Z. Wu, C. Yang, Beihang
Brazil; J. Azevedo, R. Da Silva, Aeronautics University, Beijing, China
and Space Institute (IAE), São José dos
Campos, Brazil
B. Kaiser, S. Poroseva, University of New
Mexico, Albuquerque, Albuquerque, NM
College London, London, United Kingdom
Air and Space Survivability
Structural Optimization
Fatigue and Fracture
Aeroservoelasticity and Control
1030 hrs
AIAA-2013-1484
Survivability Analysis of the
Satellite Electrical Power Subsystem
Architecture
Chaired by: R. LIND, University of Florida and P. FRIEDMANN, University of Michigan
1000 hrs
1030 hrs
0930 hrs
AIAA-2013-1486
AIAA-2013-1487
AIAA-2013-1485
Control Surface Efficiency Analysis
Robust Aeroelastic Control of Very Effects of the Aerodynamic Data
in a MIMO System Identification
and Utilization of an Elastic
Flexible Wings using Intrinsic
Framework for Aeroelastic Analyses Airplane for Maneuver Loads
Models
Y. Wang, R. Palacios, A. Wynn, Imperial J. Azevedo, Technological Institute of
Alleviation
14-SDM-5
S. Sinha, General Electric Company,
Cincinnati, OH
Chaired by: E. FAHRENTHOLD, University of Texas and J. KLOOS, GE Aviation
0930 hrs
1000 hrs
AIAA-2013-1482
AIAA-2013-1483
Transient Response of a MultiSimulation of Orbital Debris Impact
layered Composite Rotating Airfoil on Porous Ceramic Tiles
K. Son, E. Fahrenthold, University of
Under Slicing-impact Loading
13-SDM-4
Lockheed Martin Corporation, Palo Alto,
CA; C. Rankin, Rhombus Consultants
Group, Palo Alto, CA
Chaired by: S. ENGELSTAD, Lockheed Martin Corporation and S. TERMAATH, University of Tennessee
0930 hrs
1000 hrs
1030 hrs
AIAA-2013-1479
AIAA-2013-1480
AIAA-2013-1481
Optimization of Propellant Tanks Optimization of Propellant Tanks
Feasible Region of Lamination
Supported by Optimized Laminated Supported by One or Two Optimized Parameters for optimization of
Composite Tubular Struts
Laminated Composite Skirts
Variable Angle Tow (VAT) Composite
D. Bushnell, Self, Palo Alto, CA; M. Jacoby, D. Bushnell, Self, Palo Alto, CA; M. Jacoby,
Plates
12-SDM-3
A&T State University, Greensboro, NC; I. Raju, Arizona, Tucson, Tucson, AZ
NASA Langley Research Center, Hampton, VA
Chaired by: M. ENRIGHT, Southwest Research Institue and R. TAYLOR, Optimal Structures, LLC.
0930 hrs
1000 hrs
1030 hrs
AIAA-2013-1476
AIAA-2013-1477
AIAA-2013-1478
Crack Growth Prediction in Fully- Two stage damage tolerance
Fracture Mechanics Analyses for
Interface Crack Problems - A Review Coupled Thermal and Deformation evaluation of an aircraft fuselage
R. Krueger, National Institute of Aerospace,
Fields Using Peridynamic Theory
panel with a circumferential crack
Hampton, VA; K. Shivakumar, North Carolina S. Alpay, E. Madenci, University of
and a broken stringer
11-SDM-2
Beacon Hill
Berkley
Stuart
St. James
20
S. Gauthier Perron, M. Drela, Massachusetts
Institute of Technology, Cambridge, MA
J. He, Clarkson University, Potsdam, NY;
X. Guan, Siemens Corporation, Princeton,
NJ; Y. Liu, Arizona State University,
Tempe, AZ
F. Zender, D. Schrage, Georgia Institute of
Technology, Atlanta, GA; M. Richey, The
Boeing Company, Everett, WA; G. Jensen,
Brigham Young University, Provo, UT
G. Chen, Tokyo University of Science, Tokyo,
Japan; Z. Yingtao, Northwestern Polytechnical
University, Xi’an, China; J. Lu, B. Zhang, Y. Li,
Xi’an Jiao Tong University, Xi’an, China
J. El Yagoubi, G. Lubineau, S. Saghir, L.
Selvakumaran, King Abdullah University
of Science and Technology, Thuwal, Saudi
Arabia; A. Askari, A. Brown, The Boeing
Company, Seattle, WA
J. Dias, Technical University of Lisbon,
Lisbon, Portugal; A. Suleman, University of
Victoria, Victoria, Canada; B. Broughton,
CSIR, Pretoria, South Africa
Chaired by: G. CREARY, NASA Langley Research Center and D. STAGGERS, Raytheon Missile Systems
1000 hrs
1030 hrs
0930 hrs
AIAA-2013-1503
AIAA-2013-1504
AIAA-2013-1502
Wing Design as a Symphony of
Efficient Multidisciplinary
Aircraft Wind Tunnel
Geographically Dispersed, MultiAerodynamic Optimization Design
Characterization using Modern
disciplinary Undergraduate Students Based on Discrete Adjoint Method
Design of Experiments
18-SDM-9
J. Yang, W. Zhang, Y. Liu, Arizona State
University, Tempe, AZ
P. Cooley, J. Slater, Wright State
University, Dayton, OH; O. Shiryayev,
Petroleum Institute, Abu Dhabi, United
Arab Emirates
1130 hrs
AIAA-2013-1498
Improving Spectral Signature
Profiles for Fatigue Crack
Identification in Beams
L. Cavagna, S. Ricci, L. Riccobene,
Technical University of Milan, Milan, Italy
Design Process
1130 hrs
AIAA-2013-1493
Fast-GLP: a Fast Tool for the
Prediction of Worst Case Gust Loads
based on Neural Networks
Characterization and Estimation of Fatigue Life I
F. Marques dos Santos, B. Peeters, H. Van
Institute, Abu Dhabi, United Arab Emirates Der Auweraer, LMS International, Leuven,
Belgium; L. Góes, Technological Institute of
Aeronautics (ITA), São José dos Campos,
Brazil
1100 hrs
AIAA-2013-1497
Modal-Based Damage Detection
of a Composite Helicopter Main
Rotor Blade
Structural Health Monitoring I
A. Da Ronch, K. Badcock, University of
Liverpool, Liverpool, United Kingdom
Aircraft Gust I
1100 hrs
AIAA-2013-1492
A New Approach to Computational
Fluid Dynamics-Based Gust Loads
Analysis
Chaired by: K. SHIVAKUMAR, North Carolina Agricultural and Technical State University and R. NAIK, Pratt & Whitney
0930 hrs
1000 hrs
1030 hrs
AIAA-2013-1499
AIAA-2013-1500
AIAA-2013-1501
Subcycle Fatigue Crack Growth
Concurrent structural and material Experimental investigation of cyclic
Mechanism Investigation for
fatigue damage prognosis
hygrothermal aging of aircraft
Aluminum Alloys and Steel
integrating sensor data
lightning protection
17-SDM-8
E. Moehle, M. Haupt, P. Horst, Technical
University of Braunschweig, Braunschweig,
Germany
Chaired by: O. SHIRYAYEV, Petroleum Institute Abu Dhabi and V. BABUSKA, Sandia National Laboratories
0930 hrs
1000 hrs
1030 hrs
AIAA-2013-1494
AIAA-2013-1495
AIAA-2013-1496
Coupled Magnetic and Structural
Nonlinear Response Prediction of Trigonometric Collocation for
Numerical Simulation and
Cracked Rotor Based On EMD
Computation of Harmonic Response
Y. Yang, X. Ren, W. Qin, Northwestern
Experimental Validation of the
of a Cracked Beam
Polytechnical University, Xi’an, China
O. Shiryayev, B. Bakeer, Petroleum
Electro Impulse De-Icing
16-SDM-7
Chaired by: D. PITT, Boeing Engineering Operations & Technology and Y. MATSUZAKI, Nagoya University
0930 hrs
1000 hrs
1030 hrs
AIAA-2013-1489
AIAA-2013-1490
AIAA-2013-1491
Model Reduction of High-Fidelity
Membrane Wing Gust Response in Passive Gust Load Alleviation
Through Bend-Twist Coupling
Models for Gust Load Alleviation
Low Reynolds Numbers
S. Tiomkin, D. Raveh, Technion--Israel
A. Da Ronch, K. Badcock, University of
of Composite Beams on Typical
Institute of Technology, Haifa, Israel
Liverpool, Liverpool, United Kingdom
Commercial Airplane Wings
15-SDM-6
Clarendon
Charles River
Cambridge
White Hill
21
H. Lee, V. Tomar, Purdue University, West
Lafayette, IN
SDM Lecture
21-SDM-11
1300 - 1400 hrs
J. Soltis, J. Palacios, D. Wolfe, T. Eden,
Pennsylvania State University, University
Park, PA
A. Dale, J. Cooper, University of Bristol,
Bristol, United Kingdom; A. Mosquera,
Applied Computing and Engineering, Ltd.,
Daresbury, United Kingdom
C. Marks, University of Dayton Research
Institute, Dayton, OH; J. Joo, G. Reich,
Air Force Research Laboratory, WrightPatterson AFB, OH
University of Michigan, Ann Arbor, Ann
Arbor, MI
Chaired by: A. SULEMAN, University of Victoria and A. CHATTOPADHYAY, Arizona State University
1430 hrs
1500 hrs
1530 hrs
AIAA-2013-1510
AIAA-2013-1511
AIAA-2013-1512
Adaptive Camber-Morphing Wing A Reconfigurable Wing for
Synergistic Smart Morphing Aileron
A. Pankonien, C. Faria, D. Inman,
using 0-? Honeycomb
Biomimetic Aircraft
24-ASC-2
United Kingdom; N. Wereley, University of F. Previtali, A. Arrieta, P. Ermanni, Swiss
Maryland, College Park, College Park, MD; Federal Institute of Technology, Zürich,
M. Friswell, Swansea University, Swansea, Switzerland
United Kingdom
1630 hrs
AIAA-2013-1514
Performance evaluation of a 3D
morphing wing and comparison
B. Woods, Swansea University, Swansea, with a conventional wing
1600 hrs
AIAA-2013-1513
Advanced Kinematic Tailoring for
Morphing Aircraft Actuation
Morphing Structures II
Monday Afternoon Speakers’ Briefing
23-SB-2
1400 - 1430 hrs
Session Chairs and Speakers for Monday Afternoon Sessions will meet in their assigned session room
Monday Afternoon Networking Coffee Break
22-BRK-2
1400 - 1430 hrs
O. Bilgen, Old Dominion University,
Norfolk, VA; M. Friswell, Swansea
University, Swansea, United Kingdom;
D. Landman, Old Dominion University,
Norfolk, VA
1700 hrs
AIAA-2013-1515
Low Reynolds Number Behavior
of a Solid-State Piezocomposite
Variable-Camber Wing
1130 hrs
AIAA-2013-1509
Evaluation of Ice Adhesion Strength
on Erosion Resistant Materials
Genomics of Multifunctional Structures and Materials for Flight
Dan Inman
Clarence “Kelly” Johnson Professor, and Chair, University of Michigan, Ann Arbor, MI
Monday Lunch Break
20-LNCH-1
1200 - 1300 hrs
Patterson AFB, OH
S. Ghosh, V. Sundararaghavan, A. Waas,
University, Shanghai, China; Z. You, University University of Michigan, Ann Arbor, Ann
of Oxford, Oxford, United Kingdom
Arbor, MI
1100 hrs
AIAA-2013-1508
Construction of kernel for nonlocal
elasticity from one-dimensional
dispersion data in reciprocal space
Nonlinear and Nonlocal Material Response
Chaired by: W. YU and A. KELKAR, Joint School of Nanoscience & Nanoengineering
0930 hrs
1000 hrs
1030 hrs
AIAA-2013-1505
AIAA-2013-1506
AIAA-2013-1507
Understanding Effect of Grain
Computational plasticity model for
3D Finite Element Modeling of
Boundaries in the Fracture
hydrostatic pressure dependent
High-Speed Sliding Wear
R. Buentello Hernandez, A. Palazotto,
Behavior of Polycrystalline
foam materials
Air Force Institute of Technology, Wright- Tungsten under Mode-I Loading
X. Chen, H. Wang, Shanghai Jiao Tong
19-SDM-10
A. Wissa, N. Guerreiro, National Institute
of Aerospace, Hampton, VA; J. Grauer,
NASA Langley Research Center, Hampton,
VA; J. Hubbard, National Institute of
Aerospace, Hampton, VA; M. Frecker, C.
Altenbuchner, Y. Tummala, Pennsylvania
State University, University Park, PA; R.
Roberts, Air Force Research Laboratory,
Wright-Patterson AFB, OH
Statler
In Session Rooms
Plaza Ballroom
Imperial Ballroom
Lunch on Own
1730 hrs
AIAA-2013-1516
Flight Testing of Novel Compliant
Spines for Passive Wing Morphing
on Ornithopters
Imperial Ballroom
22
Laboratory, Wright-Patterson AFB, OH
Institute of Technology, Pasadena, CA
S. Jeon, Moog-CSA Engineering,
Albuquerque, NM; T. Murphey, Air Force
Research Laboratory, Kirtland AFB,
NM; E. Ardelean, Schafer Corporation,
Albuquerque, NM
J. Sobotka, University of Illinois, UrbanaChampaign, Urbana, IL; A. Oral, Yildiz
Technical University, Istanbul, Turkey; A. Culler,
Universal Technology Corporation, Dayton, OH
Zürich, Zürich, Switzerland
Blacksburg, VA; R. Snyder, Air Force
Research Laboratory, Kirtland AFB, NM
G. Kennedy, J. Martins, University of
Michigan, Ann Arbor, Ann Arbor, MI
Chaired by: M. BHATIA, Virginia Tech and G. SINGH, General Electric - Global Research
1500 hrs
1530 hrs
1430 hrs
AIAA-2013-1529
AIAA-2013-1530
AIAA-2013-1528
Aero-Structural Optimization of 3-D Aeroelastic Shape Optimization of a An Adjoint-based Derivative
Adaptive Wings with Embedded
Flapping Wing
Evaluation Method for TimeE. Stewart, M. Patil, R. Canfield, Virginia dependent Aeroelastic Optimization
Smart Actuators
Polytechnic Institute and State University, of Flexible Aircraft
G. Molinari, A. Arrieta, P. Ermanni, ETH
27-MDO-2
L. Datashvili, H. Baier, B. Wei, S. Endler,
Technical University of Munich, Garching,
Germany; L. Schreider, Thales Alenia
Space, Toulouse, France
Chaired by: G. DAVIS, Jet Propulsion Laboratory and M. SANTER, Imperial College London
1430 hrs
1500 hrs
1530 hrs
AIAA-2013-1522
AIAA-2013-1523
AIAA-2013-1524
Design of a Morphing Skin Using Ultra-Thin Highly Deformable
Structural determinancy and design
Flexible Fiber Composites for
Composite Mirrors
implications for tensioned precision
J. Steeves, S. Pellegrino, California
Space-Reconfigurable Reflectors
deployable structures
26-GSF-2
Corporation, Dayton, OH; J. Hollkamp,
B. Tojo, A. Marta, Technical University of
Lisbon, Lisbon, Portugal
1600 hrs
AIAA-2013-1531
Aero-Structural Blade Design of a
High-Power Wind Turbine
Aero-Structural Optimization
S. Bradford, Jet Propulsion Laboratory,
California Institute of Technology, Pasadena,
CA; W. Wilkie, NASA Langley Research Center,
Hampton, VA; G. Agnes, L. Peterson, Jet
Propulsion Laboratory, California Institute of
Technology, Pasadena, CA
1600 hrs
AIAA-2013-1525
Controlling Wavefront in
Lightweight Reflector Systems using
Piezocomposite Actuator Arrays
Large Area Space Structures
X. Wang, R. Perez, M. Mignolet, Arizona
State University, Tempe, AZ
1600 hrs
AIAA-2013-1520
Nonlinear Reduced Order Modeling
of Complex Wing Models
H. Shi, B. Yang, University of Southern
California, Los Angeles, CA; H. Fang,
Shanghai Yue-Sheng Technology, Inc.,
Shanghai, China
1630 hrs
AIAA-2013-1526
Offset-Feed Surface Mesh
Generation for Design of Space
Deployable Mesh Reflectors
R. Kuether, M. Allen, University of
Wisconsin, Madison, Madison, WI
1630 hrs
AIAA-2013-1521
Nonlinear Modal Substructuring
of Systems with Geometric
Nonlinearities
Multidisciplinary Analysis for Combined Environment Structures I
Chaired by: J. SLATER, Wright State University and B. WHITING, The Boeing Company
1430 hrs
1500 hrs
1530 hrs
AIAA-2013-1517
AIAA-2013-1518
AIAA-2013-1519
Towards a Coupled Loads-ResponseA Coupled Approach for Modeling Modeling Damage Within a
Reduced-Order Model Framework: Life Prediction Framework for
Damage within a ReducedAn Application
Hypersonic Structures in Combined
OrderModel Framework
P. O’Hara, Universal Technology
J. Hollkamp, P. O’Hara, Air Force Research Extreme Environments
25-DSC-2
T. Hodges, J. Blandino, D. Rochow,
Virginia Military Institute, Lexington, VA
1700 hrs
AIAA-2013-1527
Temperature Dependent Frequency
Response of a Constant Tension
Membrane
Cabot
Thoreau
Lexington
23
A. Deshmukh, J. Allison, University of
Illinois, Urbana-Champaign, Urbana, IL
Technologies, Inc., Moffett Field, CA; K.
Goebel, NASA Ames Research Center,
Moffett Field, CA
D. Villanueva, University of Florida,
Gainesville, Gainesville, FL; R. Le Riche,
G. Picard, École Nationale Supérieure des
Mines de Saint-Étienne, Saint-Étienne,
France; R. Haftka, University of Florida,
Gainesville, Gainesville, FL
1530 hrs
AIAA-2013-1534
Dynamic Design Space Partitioning
for Optimization of an Integrated
Thermal Protection System
S. Mahadev, W. Chan, University of Texas, Technical University of Turin, Turin, Italy
Arlington, Arlington, TX
Command, San Diego, CA; S.
Venkataraman, San Diego State
University, San Diego, CA
G. Steckel, The Aerospace Corporation, El
Segundo, CA
Z. Kier, A. Waas, University of Michigan,
Ann Arbor, Ann Arbor, MI
Chaired by: J. ROME, The Aerospace Corporation and T. LACY, Mississippi State University
1500 hrs
1530 hrs
1430 hrs
AIAA-2013-1546
AIAA-2013-1547
AIAA-2013-1545
Numerical Investigation of Tapered Strength of Composite Foam Core Determining Effective Interface
Sandwich Closeouts with Isotropic Sandwich Structures Subjected to Fracture Properties of 3D Fiber
Thermomechanical Loading
Reinforced Foam Core Sandwich
Functionally Graded Cores
K. Wagschal, Naval Air Systems
C. Foerster, V. Goyal, J. Rome, D. Patel, Structures
31-SDM-13
Tucson, Tucson, AZ; A. Tessler, NASA Langley
Research Center, Hampton, VA
Chaired by: C. BISAGNI, Politecnico Di Milano and M. ROYBAL, Raytheon Missile Systems
1500 hrs
1530 hrs
1430 hrs
AIAA-2013-1540
AIAA-2013-1541
AIAA-2013-1539
Prediction of Composite Laminate Closed-Form Analytical Method
Evaluation of Failure Parameters
Strength Properties Using a Refined for Analyzing Laminated
in Composite Structures by
Zigzag Plate Element
Composite Tubes in Hygrothermal Component-Wise Approach
A. Barut, E. Madenci, University of Arizona,
E. Carrera, M. Maiaru, M. Petrolo,
Environment
30-SDM-12
M. Razi, P. Attar, P. Vedula, University of
Oklahoma, Norman, Norman, OK
A. Virakthi, S. Lee, S. Haldar, H. Bruck,
University of Maryland, College Park,
College Park, MD; A. Rahman, Naval Air
Systems Command, Patuxent River, MD
1600 hrs
AIAA-2013-1548
Modeling of pin-facesheet interactions
in k-cor sandwich structures under
compressive loading
Sandwich Structures
N. Nguyen Sy, J. Lee, M. Cho, Seoul
National University, Seoul, South Korea
1600 hrs
AIAA-2013-1542
Efficient higher order plate theory
for viscoelastic composite laminates
Composites: Analytical Methods I
Non-Deterministic Methods II
C. Bakker, G. Parks, J. Jarrett, University
of Cambridge, Cambridge, United Kingdom
1600 hrs
AIAA-2013-1535
Differential Geometry and Design
Coupling in MDO
A. Christensen, B. Sens, S. James,
S. Venkataraman, San Diego State
1630 hrs
AIAA-2013-1549
Experimental Investigation of
Tapered Edge Closeouts in Sandwich
Composite Panels
Stuart
St. James
Winthrop
1730 hrs
AIAA-2013-1551
Failure Prediction in Sandwich
Panels under Blast Loading Using a
Refined Zigzag Element
Constitution
B. Hasseldine, A. Zehnder, B. Keating,
Cornell University, Ithaca, NY; A. Singh, B. M. Dorduncu, A. Barut, E. Madenci,
Davidson, Syracuse University, Syracuse, University of Arizona, Tucson, Tucson, AZ
NY
1700 hrs
AIAA-2013-1550
Compression After Impact of Thick
Sandwich Composite Structures
1700 hrs
AIAA-2013-1544
Effect of Viscoelastic Interface on
the Behavior of Nanocomposites
Z. Hasan, A. Chattopadhyay, Y. Liu,
Arizona State University, Tempe, AZ
M. Kobayashi, University of Hawaii,
Manoa, Honolulu, HI; M. Nikbay, Istanbul
Technical University, Istanbul, Turkey
1630 hrs
AIAA-2013-1543
On a Fourier Spectral Variational
Asymptotic Method for Cellular
Optimization Frameworks and Applications
Chaired by: S. POROSEVA, The University of New Mexico and B. THACKER, Southwest Research Institue
1430 hrs
1500 hrs
1530 hrs
AIAA-2013-1536
AIAA-2013-1537
AIAA-2013-1538
Uncertainty Quantification for
Uncertainty Quantification in
Uncertainty Propagation Using
Multidimensional Dynamical
Remaining Useful Life of Aerospace Random Eigenfunction Expansion
Systems Based on Adaptive
Components using State Space
Method
S. Adhikari, Swansea University, Swansea,
Numerical Solution of Liouville
Models and Inverse FORM
United Kingdom
S. Sankararaman, Stinger Ghaffarian
Equation
29-NDA-2
California, Berkeley, Berkeley, CA
Chaired by: V. TOROPOV, University of Leeds and J. CHRISSIS, USAF
1430 hrs
1500 hrs
AIAA-2013-1532
AIAA-2013-1533
Simultaneous Structural and
Fast Wind Turbine Design via
Control System Design for
Geometric Programming
W. Hoburg, P. Abbeel, University of
Horizontal Axis Wind Turbines
28-MDO-3
24
of Lisbon, Porto, Portugal; M. Moura,
University of Porto, Porto, Portugal
J. Hobeck, M. Obenchain, University of
Y. Zhimiao, A. Abdelkefi, M. Hajj, Virginia
Blacksburg, VA
B. Owens, J. Weber, B. Yancey, L. Zhuang,
R. Talreja, Texas A&M University, College
Station, TX
N. Sivaneri, West Virginia University,
Morgantown, WV
1600 hrs
AIAA-2013-1567
Hygrothermal Effect of Composite
Beams Subjected to Moving Loads
Beam Dynamics I
1630 hrs
AIAA-2013-1561
Vibration Testing of Aeroelastic
Structures Containing Geometric
Stiffness Nonlinearities
J. Sodja, R. Drazumeric, T. Kosel,
G. Charmbalis, J. Cooper, University of
University of Ljubljana, Ljubljana, Slovenia; Bristol, Bristol, United Kingdom
P. Marzocca, Clarkson University, Potsdam,
NY
1600 hrs
AIAA-2013-1560
Aeroelastic Design of Propellers
with Optimized Load-Distribution
Characteristics
C. Xie, Y. Liu, C. Yang, Beihang University, Institute of Technology, Atlanta, GA
Beijing, China
P. Mardanpour, P. Richards, O. Nabipour, D.
Hodges, Georgia Institute of Technology,
Atlanta, GA
1600 hrs
AIAA-2013-1571
Effect of Multiple Engine Placement
on Aeroelastic Trim and Stability of
Flying Wing Aircraft
Y. Bichiou, Virginia Polytechnic Institute and
State University, Blacksburg, VA; A. Nuhait,
King Saud University, Riyadh, Saudi Arabia;
A. Abdelkefi, M. Hajj, Virginia Polytechnic
1700 hrs
AIAA-2013-1562
Unsteady Aeroelastic Response of
Rigid Airfoils with Nonzero Angles
of Attack
1630 hrs
AIAA-2013-1556
Sustainability Assessment of a Wind
Turbine Blade: An Engineering
Framework
Energy Harvesting and Aeroservoelasticity Design
1530 hrs
AIAA-2013-1566
A Rayleigh-Ritz Model for Dynamic
Response and Buckling Analysis
of Delaminated Composite
H. Akhavan, P. Ribeiro, Technical University Timoshenko Beams
1500 hrs
AIAA-2013-1565
Composite laminates with linearly
varying fiber angles under static
and dynamic loads
L. Demasi, R. Cavallaro, San Diego State
Chaired by: F. NITZSCHE, Carleton University and J. MCNAMARA, The Ohio State University
1500 hrs
1530 hrs
1430 hrs
AIAA-2013-1569
AIAA-2013-1570
AIAA-2013-1568
Nonlinear analysis of piezoelectric Aeroelastic Trim Analysis of Very Passive Morphing of Flying Wing
Flexible Aircraft Based on 3-D
Aircraft - Part I: Z Configuration
energy harvesters from ambient
P. Mardanpour, D. Hodges, Georgia
Lifting-Line Theory
and galloping vibrations
35-SDM-17
J. Kim, Kumoh National Institute of
Technology, Gumi, South Korea
Chaired by: J. KOSMATKA
1430 hrs
AIAA-2013-1564
A Dynamic Model for Thin-Walled
Composite Beams via Asymptotic
Strain Energy Transformation
34-SDM-16
Stasiunas, Sandia National Laboratories,
R. Cavallaro, L. Demasi, San Diego State
Albuquerque, NM; J. Freymiller, ATA
Engineering, Inc., Albuquerque, NM; M. Lawry,
University of Colorado, Boulder, Boulder, CO
V. Suryakumar, T. Strganac, Texas A&M
University, College Station, TX
1600 hrs
AIAA-2013-1555
A Finite element-Multibody
dynamics co-simulation
methodology applied to FAST
Aircraft Design and Nonlinear Dynamics
Chaired by: M. ROSS, Sandia National Laboratories and J. COOPER, University of Bristol
1430 hrs
1500 hrs
1530 hrs
AIAA-2013-1557
AIAA-2013-1558
AIAA-2013-1559
Simulating the Response of
Risks of Linear Design of Joined
Post-Critical Analysis of Joined
External Stores on Aircraft Using Wings: a Nonlinear Dynamic
Wings: the Concept of SnapLinear and Nonlinear Vibroacoustics Perspective in the Presence of
Divergence as a Characterization of
M. Ross, T. Walsh, J. Rouse, D. Tipton, E.
Follower Forces
the Instability
33-SDM-15
University, College Station, TX; J.
Paquette, D. Griffith, M. Barone, Sandia
National Laboratories, Albuquerque, NM
1530 hrs
AIAA-2013-1554
Carbon Design Studies for Large
Blades: Performance and Cost
Tradeoffs for the Sandia 100-meter
Wind Turbine Blade
Wind Turbine Dynamics, Loads, and Control
D. Griffith, W. Johanns, Sandia National
M. Benedict, J. Pino, I. Chopra, University Laboratories, Albuquerque, NM
of Maryland, College Park, College
Park, MD
Chaired by: D. GRIFFITH and B. RESOR, Sandia National Laboratories
1430 hrs
1500 hrs
AIAA-2013-1552
AIAA-2013-1553
Aeroelastic Modeling of Large Off- Fundamental Understanding of the
shore Vertical-axis Wind Turbines: Physics of a Small-Scale Vertical
Development of the Offshore Wind Axis Wind Turbine with Dynamic
Energy Simulation Toolkit
Blade Pitching: An Experimental
B. Owens, J. Hurtado, Texas A&M
and Computational Approach
32-SDM-14
Cambridge
White Hill
C. Eger, A. Ricciardi, R. Canfield, M. Patil,
University, Blacksburg, VA
Beacon Hill
1730 hrs
AIAA-2013-1563
Design of a Scaled Flight Test
Vehicle Including Linear Aeroelastic
Effects
Berkley
25
South Carolina, Columbia, Columbia, SC
H. Millwater, D. Wagner, J. Garza, A.
Baines, K. Lovelady, University of Texas,
San Antonio, San Antonio, TX
R. Williams, Raytheon Company, El
Segundo, CA; C. Fisher, J. Gallon, Jet
Propulsion Laboratory, California Institute
of Technology, Pasadena, CA
1530 hrs
AIAA-2013-1574
Practical Considerations for using
Constant Force Springs in SpaceBased Mechanisms
Digital Twin I
A. Adomeit, H. Reimerdes, M.
Lakshmanan, T. Schervan, A. Dafnis,
RWTH Aachen University, Aachen,
Germany
1600 hrs
AIAA-2013-1575
Structural Concept and Design for
Modular and Serviceable Spacecraft
Systems
Design: Spacecraft I
T. Li, W. Zuowei, H. Deng, Xidian
University, Xi’an, China
1630 hrs
AIAA-2013-1576
Mesh reflector antennas: formfinding analysis review
Hungarian Academy of Sciences,
Budapest, Hungary
E. Sengezer, G. Seidel, Virginia Polytechnic
Colombini, B. Wardle, Massachusetts
Chaired by: S. ROY, The University of Alabama; J. KOO, The University of Texas at Austin
1430 hrs
1500 hrs
1530 hrs
AIAA-2013-1581
AIAA-2013-1582
AIAA-2013-1583
Processing and Characterization
Phenomenological Characterization Processing and Mechanical
of Cyanate Ester-MWNT
of the Fabrication of Aligned
Property Characterization of
Nanocomposites
Carbon Nanotube Nanocomposites Aligned Carbon Nanotube Carbon
S. Lao, T. Moon, J. Koo, University of
via Dielectrophoresis Under AC
Matrix Nanocomposites
Texas, Austin, Austin, TX; Z. Horvath,
I. Stein, H. Vincent, S. Steiner, E.
Electric Field
38-SDM-20
Reifsnider, University of South Carolina,
Columbia, Columbia, SC
J. Koo, University of Texas, Austin,
Austin, TX; J. Lee, Agency for Defense
Development, Daejeon, South Korea; L.
Pilato, KAI, Inc., Austin, TX
1600 hrs
AIAA-2013-1584
Methodology for Assessment
of Morphological and Thermal
Characteristics of Nanographene
Platelets
Nanostructured Materials I
San Antonio, San Antonio, TX
D. Drake, J. Simsiriwong, R. Sullivan, H.
Toghiani, S. Nouranian, J. DuBien, T. Lacy,
C. Pittman, Mississippi State University,
Mississippi State, MS
1630 hrs
AIAA-2013-1585
Creep Compliance Characterization of
Vapor-Grown Carbon Nanofiber/Vinyl
Ester Nanocomposites Using a Central
Composite Design of Experiments
Chaired by: E. GLAESSGEN, NASA Langley Research Center; J. RANSOM, NASA Langley Research Center and D. STARGEL, AF Office of Scientific Research
1430 hrs
1500 hrs
1530 hrs
1600 hrs
AIAA-2013-1577
AIAA-2013-1578
AIAA-2013-1579
AIAA-2013-1580
Multi-physics Response of Structural Multiphysics Stimulated Simulation Application of the Complex Variable Sensitivity Analysis in Structural
Composites and Framework for
Digital Twin Methods for Fleet
Finite Element Method, ZFEM, to
Dynamics using the ZFEM Complex
Modeling Using Material Geometry Management
Structural Mechanics Sensitivity
Variable Finite Element Method
P. Majumdar, M. FaisalHaider, K.
K. Reifsnider, P. Majumdar, University of Analysis
J. Garza, H. Millwater, University of Texas,
37-SDM-19
M. Contreras, B. Trease, Jet Propulsion
Laboratory, California Institute of Technology,
Pasadena, CA; C. Bojanowski, R. Kulak,
Argonne National Laboratory, West Chicago, IL
Chaired by: C. HALL, North Carolina State University and M. BAILEY, GE
1430 hrs
1500 hrs
AIAA-2013-1572
AIAA-2013-1573
Characterizing Wheel-Soil Interaction Structural Design and History
Loads Using Meshfree Finite Element of the Hexagon Reconnaissance
Camera
Methods: A Sensitivity Analysis for
P. Pressel, Self, San Diego, CA
Design Trade Studies
36-SDM-18
N. Jahan, M. Hosur, S. Jeelani, Tuskegee
University, Tuskegee, AL
1700 hrs
AIAA-2013-1586
Low-Velocity Impact Response of
Woven Carbon Epoxy Composites
with MWCNTs
R. Santhanakrishnan, Anna University,
Chennai, India
Imperial Ballroom
Clarendon
1730 hrs
AIAA-2013-1587
Evaluation Strength of Stitched
Foam Sandwich Structures
Charles River
26
Additive Manufacturing
Franklin
44-BRK-3
0900 - 0930 hrs
43-NDA-3
0800 - 0900 hrs
Non-Deterministic Approaches (NDA) Keynote
Tuesday Morning Speakers’ Briefing
Tuesday Networking Coffeee and Pastries
Tuesday
Welcome Reception
Tuesday Morning Networking Coffee Break
Assuring Aero-Structural Reliability in an Uncertain World
Ravi Chona
USAF Senior Scientist and Director, Structural Sciences Center, Air Force Research Laboratory, Wright-Patterson AFB, OH
Session Chairs and Speakers in Tuesday Morning sessions will meet in their assigned session room.
42-SB-3
0730 - 0800 hrs
41-NB-2
0700 - 0800 hrs
40-RCPT-1
1800 - 1930 hrs
Moderators: Dr. Paul McManamon, Air Force Research Laboratory, Chief Scientist for Sensors, Retired, and Dr. Joseph H. Koo, University of Texas, Austin
Panelists:
3D Printing, Additive Manufacturing, and Solid Freeform
Investigating Process Maturity in Aerospace Additive Manufacturing
Boeing’s Involvement on Additive Manufacturing
Fabrication: A New Direction in Manufacturing
Dr. Mark D. Benedict
Orval M. “Jack” Nobles
Professor Joseph J. Beaman
Materials Engineer, Air Force Research Laboratory
The Boeing Company, Boeing Research & Technology
University of Texas at Austin, Dept. of Mechanical Engineering
St. Louis, MO
Austin, TX
Plaza Ballroom
Imperial Ballroom
In Session Rooms
Plaza Ballroom
Georgian Ballroom
The Role of the Additive Manufacturing Institute
Ed Morris
Director, National Additive Manufacturing Innovation Institute (NAMII)
Vice President, National Center for Defense Manufacturing and
Machining (NCDMM)
Youngstown. OH
Additive Manufacturing is revolutionizing manufacturing. It is the cutting edge for advanced manufacturing. It has recently been highlighted in the National Academy of Sciences report, Optics and Photonics; Essential Technologies for our Nation, co-chaired by Dr McManamon,
a co-chair of this panel. Additive Manufacturing is especially important for aerospace applications because of requirements for specialized, custom parts that need to be made in low quantities. This panel discussion will highlight developments and perspectives in additive
manufacturing for aerospace application. Additive manufacturing will be critical to the aerospace industry for specialized parts only available using additive manufacturing, and for cost reduction.
39-SDM-21
1430 - 1700 hrs
27
G. Huff, S. Long, F. Drummond, N.
Brennan, A. Couch, Texas A&M University,
College Station, TX
China
J. Denhart, T. Gemmer, S. Ferguson, A.
J. Hwang, D. Lee, J. Cutler, J. Martins,
Mazzoleni, North Carolina State University, University of Michigan, Ann Arbor, Ann
Raleigh, NC
Arbor, MI
O. Bendiksen, University of California, Los
Angeles, Los Angeles, CA
Hypersonics II
1100 hrs
AIAA-2013-1593
Transonic Single-Degree-ofFreedom Flutter and Natural Mode
Instabilities
Space Applications
of Cambridge, Cambridge, United Kingdom
J. Coimbra, A. Marta, Technical University
of Lisbon, Lisbon, Portugal
1100 hrs
AIAA-2013-1601
Aero-Acoustic Optimization of
Airfoils for Wind Turbines
Optimization Applications II
M. Natori, N. Katsumata, Waseda
J. Hinkle, C. Willey, ILC Dover, Frederica,
University, Shinjuku, Japan; N. Okuizumi, DE; D. Kling, Folded Structures Company,
Japan Aerospace Exploration Agency
Ringoes, NJ
(JAXA), Sagamihara, Japan; A. Watanabe,
Sakase Adtech Company, Ltd., Sakai,
Japan; H. Yamakawa, Waseda University,
Shinjuku, Japan
1100 hrs
AIAA-2013-1597
Numerical Study and Design of
Foldable and Expandable Space
Structures
Membrane Packaging and Applications
Chaired by: A. KO, Phoenix Integration, Inc. and R. KHIRE, United Technologies Research Center
1000 hrs
1030 hrs
0930 hrs
AIAA-2013-1599
AIAA-2013-1600
AIAA-2013-1598
Large-Scale MDO of a Small
Tailored Seeding Geometries
Tradespace Exploration of
Reconfigurability using Surrogate Satellite using a Novel Framework for the Multi-Fidelity Design of
for the Solution of Coupled Systems Compression Systems
Points to Simplify Dominance
J. Eastwood, T. Ghisu, J. Jarrett, University
and their Derivatives
Determination
48-MDO-4
of Technology, Pasadena, CA; R. Danner, Y. Satou, H. Furuya, Tokyo Institute of
Northrop Grumman Corporation, Redondo Technology, Yokohama, Japan
Beach, CA
Chaired by: W. WILKIE, NASA Langley Research Center and J. FOOTDALE, Load Path, LLC
0930 hrs
1000 hrs
1030 hrs
AIAA-2013-1594
AIAA-2013-1595
AIAA-2013-1596
Origami Sunshield Concepts for
Fold Line Based on Mechanical
Deployable Membrane Structures
Space Telescopes
Properties of Crease in Wrapping with Rolled-up Booms and Their
L. Wilson, S. Pellegrino, California Institute Fold Membrane
Deployment Characteristics
47-GSF-3
S. He, Y. Gu, Z. Yang, Northwestern
Polytechnical University, Xi’an, China
Chaired by: R. SCOTT, NASA Langley Research Center and J. ROGERS, Lockheed Martin Corporation
0930 hrs
1000 hrs
1030 hrs
AIAA-2013-1590
AIAA-2013-1591
AIAA-2013-1592
Analysis of Transonic Limit Cycle
Aerothermoelastic and Aeroelastic Aerothermal Mode and Dynamic
Oscillation Using Aerodynamic
Studies of Hypersonic Vehicles
Analysis of Hypersonic Vehicle
H. Chen, J. Wang, H. Chen, University of
Describing Functions and
using CFD
Science and Technology of China, Hefei,
N. Lamorte, P. Friedmann, University of
Superposition Principle
46-DSC-3
Chaired by: F. ABDI, AlphaSTAR Corporation
0930 hrs
1000 hrs
AIAA-2013-1588
AIAA-2013-1589
Evaluation of Fluidic-Based
Variable Thermal Conductivity,
Contact-Aided Cellular Structures Mechanisms for Electromagnetic
Compensation from Mechanical
for Spacecraft Thermal Control
R. Stavely, G. Lesieutre, Pennsylvania
Bending and Thermoregulation of
State University, University Park, PA
Flexible Patch Antenna
45-ASC-3
Cabot
Thoreau
Lexington
Statler
28
J. Ocampo, H. Millwater, University of
Texas, San Antonio, San Antonio, TX
Logan, UT
S. Wicks, B. Wardle, Massachusetts
Arbor, Ann Arbor, MI; E. Pineda, NASA
Glenn Research Center, Cleveland, OH; C.
Henrich, Sogeti Germany GmbH, Hamburg,
Germany; A. Waas, University of Michigan,
Chaired by: J. MIN, NASA Glenn Research Center and A. NAJAFI, ANSYS, Inc.
0930 hrs
1000 hrs
AIAA-2013-1612
AIAA-2013-1613
Interlaminar Fracture Toughness
A Unified Model for Predicting the
of Laminated Woven Composites
Open Hole Tensile and Compressive
Reinforced with Aligned Nanoscale Strengths of Composite Laminates
Fibers: Mechanisms at the Macro, for Aerospace Applications
P. Davidson, University of Michigan, Ann
Micro, and Nano Scales
51-SDM-23
M. Sunny, C. Sultan, R. Kapania, Virginia
Blacksburg, VA
Chaired by: W. YU and T. MANN, NASA Langley Research Center
0930 hrs
1000 hrs
AIAA-2013-1607
AIAA-2013-1608
Optimal Energy Harvesting From A Homogenization of Piecewise
Membrane Attached To A Tensegrity Straight Corrugated Plates
Z. Ye, W. Yu, Utah State University,
Structure
50-SDM-22
Beach, CA
Torng, The Boeing Company, Chicago, IL
H. Pollayi, W. Yu, Utah State University,
Logan, UT
1030 hrs
AIAA-2013-1614
Modeling Matrix Cracking in
Composite Rotor Blades within
VABS Framework
M. Atri, C. Upadhyay, R. Dhama, Indian
Institute of Technology Kanpur, Kanpur,
India
1030 hrs
AIAA-2013-1609
Identification of Damage and
Damage Parameters in Structures
using Daubechies Wavelets with
Spectral Element Method
J. Kwak, H. Cho, S. Shin, Seoul National
University, Seoul, South Korea; O. Bauchau,
University of Michigan and Shanghai Jiao Tong
University Joint Institute, Shanghai, China
L. He, H. Huang, S. Zhu, D. Ling,
University of Electronic Science and
Technology of China, Chengdu, China
1130 hrs
AIAA-2013-1606
Uncertainty quantification in
fatigue lifetime data analysis: a
possibilistic approach
1130 hrs
AIAA-2013-1616
Effect Of Coupling Of Damage
Mechanisms In The Degradation
Model Of Composite Laminates
A. Lal, R. Kapania, Virginia Polytechnic Institute R. Dhama, C. Upadhyay, V. Murari, Indian
and State University, Blacksburg, VA
Institute of Technology Kanpur, Kanpur,
India
1100 hrs
AIAA-2013-1615
Stochastic Critical Stress Intensity
Factor Response of Single Edge
Notched Laminated Composite Plate
Composites: Fatigue and Fracture I
1130 hrs
AIAA-2013-1611
Analysis of two-dimensional improved
finite element domain decomposition
A. Rajagopal, D. Hodges, Georgia Institute method using local and mixed
of Technology, Atlanta, GA
Lagrange multipliers
1100 hrs
AIAA-2013-1610
Asymptotic Approach to Oblique
Cross-Sectional Analysis of Beams
Analytical Methods for Structures II
S. Das, S. Chakravarty, University at
Buffalo, Buffalo, NY
1100 hrs
AIAA-2013-1605
Characterization of microanomalies from macro-scale
response
Non-Deterministic Fatigue and Fracture
Chaired by: M. ENRIGHT, Southwest Research Institue and S. KUMARI, Pratt & Whitney-Rocketdyne
0930 hrs
1000 hrs
1030 hrs
AIAA-2013-1602
AIAA-2013-1603
AIAA-2013-1604
Probabilistic Damage Tolerance for Single Flight Probability of Failure
A Confidence Bound Approach
in Probabilistic Damage Tolerance
for Fatigue Failure Prediction and Small Airplanes Using a LinearElastic Crack Growth Fracture
Analysis
Forecasting
T. Torng, The Boeing Company, Huntington Mechanics Surrogate Model
K. Halbert, L. Fitzwater, H. Smith, T.
49-NDA-4
St. James
Constitution
Winthrop
29
K. Woo, J. Nelson, D. Cairns, T. Riddle,
Montana State University, Bozeman, MT
of Lisbon, Lisbon, Portugal
M. McWilliam, S. Lawton, M. Fluck,
G. Mustafa, C. Crawford, University of
Victoria, Victoria, Canada
1030 hrs
AIAA-2013-1629
An implicit model for Lagrangian
vortex dynamics for Horizontal
Axis Wind Turbine design
optimization
B. Plaumann, O. Rasmussen, D. Krause,
Hamburg University of Technology,
Hamburg, Germany
London, London, United Kingdom
1100 hrs
AIAA-2013-1635
Aeroelastic Analysis of a Folding
Wing: Comparison of Simple and
Higher Fidelity Models for a Wide
R. Simpson, R. Palacios, Imperial College Range of Fold Angles
I. Wang, S. Gibbs IV, E. Dowell, Duke
University, Durham, NC
Aircraft Dynamics
J. Mandell, D. Miller, D. Samborsky,
1100 hrs
AIAA-2013-1630
Creep/Fatigue Behavior of Resin
Infused Biaxial Glass Fabric
Laminates
K. Tamma, A. Hoitink, M. Shimada, University
of Minnesota, Minneapolis, Minneapolis, MN
1130 hrs
AIAA-2013-1636
On the Significance of a Novel
Midpoint Rule with Midpoint
Acceleration Technique for Index 3
DAE Multibody Dynamical Systems
C. Crawford, G. Mustafa, University of
Victoria, Victoria, Canada
1130 hrs
AIAA-2013-1631
Micromechanics Investigation
of Wind Turbine Blade Fatigue
Behavior Considering Multi-Axial
Loading
Wind Turbine Blade Composite Material Analysis and Testing
Chaired by: C. CESNIK, University of Michigan, Media Union Library and V. WICKRAMASINGHE
1000 hrs
1030 hrs
0930 hrs
AIAA-2013-1633
AIAA-2013-1634
AIAA-2013-1632
Fundamental Bending Frequencies Numerical aspects of nonlinear
System analysis and synthesis
of Tapered Wings
flexible aircraft flight dynamics
for the dimensioning of variant
L. Campos, A. Marta, Technical University modeling
lightweight cabin interior
55-SDM-27
Chaired by: D. CAIRNS, Montana State University and J. MANDELL
1000 hrs
0930 hrs
AIAA-2013-1628
AIAA-2013-1627
Effects of Defects Part A: Stochastic Effects of Defects: Part B—
Finite Element Modeling of Wind
Progressive Damage Modeling
Turbine Blades with Manufacturing of Fiberglass/Epoxy Composite
Structures with Manufacturing
Defects for Reliability Estimation
T. Riddle, D. Cairns, J. Nelson, Montana
Induced Flaws Utilizing Cohesive
State University, Bozeman, MT
Zone Elements
54-SDM-26
Z. Hasan, Arizona State University,
F. Yuan, R. Chapman, North Carolina State Z. Esau, K. McCullough, K. Montel, M. Cosmo,
Tempe, AZ; G. Atmeh, University of Texas, University, Raleigh, NC
D. Rhymer, U.S. Air Force Academy, Colorado
Arlington, Arlington, TX
Springs, CO; D. Cope, C. Thwing, Southwest
Research Institute, San Antonio, TX
1130 hrs
AIAA-2013-1626
Modeling of an Arch Dam LongTerm Static Deformation for
Structural Health Monitoring
K. Lee, Singapore University of Technology J. Lew, Tennessee State University,
and Design, Singapore, Singapore;
Nashville, TN; C. Loh, National Taiwan
K. Willcox, Massachusetts Institute of
University, Taipei, Taiwan
Technology, Cambridge, MA
1100 hrs
AIAA-2013-1625
Structural Integrity Assessment via
Structural Response Predictions using
a Certified Reduced Basis Model
1030 hrs
AIAA-2013-1624
Fatigue Test of Fuselage Longerons
with Magnetostrictive Sensor
Monitoring System
1130 hrs
AIAA-2013-1621
Towards mechanisms-guided
resistivity-based monitoring of
damage in laminated composites
Z. YU, P. Yi, H. Wang, Shanghai Jiao Tong G. Lubineau, King Abdullah University of
University, Shanghai, China
Science and Technology, Thuwal, Saudi
Arabia
Structural Health Monitoring II
University of Florida, Gainesville,
Gainesville, FL; R. Goldberg, NASA Glenn
Research Center, Cleveland, OH
Chaired by: J. ZIPAY, NASA Johnson Space Center and H. HILTON
0930 hrs
1000 hrs
AIAA-2013-1622
AIAA-2013-1623
Conceptual Implementation of
Damage Detection in a Hybrid
an Automated Structural Health
Composite Panel Using Arrays of
Monitoring System
Piezoelectric Actuators/Sensors
C. Cater, Michigan State University, East
Lansing, MI; R. Goldberg, NASA Glenn
Research Center, Cleveland, OH; X. Xiao,
Michigan State University, East Lansing,
MI; L. Kohlman, NASA Glenn Research
Center, Cleveland, OH
53-SDM-25
of Iowa, Iowa City, Iowa City, IA
1100 hrs
AIAA-2013-1620
Low-Velocity Impact Test of a
Composite Wing Box and Analytical
Prediction of Contact Indentation
Composites: Impact, Damage, and Voids
Chaired by: S. RUSSELL, Triumph Aerostructures and M. RASSAIAN, Boeing Engineering Operations & Technology
0930 hrs
1000 hrs
1030 hrs
AIAA-2013-1617
AIAA-2013-1618
AIAA-2013-1619
Quantifying Effects of Voids in
Impact Response of CFRP laminates Improived Subcell Model for the
Prediction of Braided Composite
Woven Ceramic Matrix Composites
with CNT buckypaper layers
C. Hill, Y. Wang, O. Zhupanska, University Response
M. Goldsmith, B. Sankar, R. Haftka,
52-SDM-24
White Hill
Berkley
Franklin
Stuart
30
H. Khodaparast, University of Liverpool,
Liverpool, United Kingdom; J. Cooper,
University of Bristol, Bristol, United Kingdom
M. Kulkarni, M. Patil, Virginia Polytechnic A. Gogulapati, P. Friedmann, J. Martins,
Institute and State University, Blacksburg, University of Michigan, Ann Arbor, Ann
VA; R. Snyder, Air Force Research
Arbor, MI
S. Zhu, H. Huang, University of Electronic
Science and Technology of China, Chengdu,
China; R. Smith, V. Ontiveros, University of
Maryland, College Park, College Park, MD;
L. He, University of Electronic Science and
Technology of China, Chengdu, China; M.
Modarres, University of Maryland, College
Park, College Park, MD
and Technology Research Institute, Beijing, Tempe, AZ
China; L. Wang, Peking University, Beijing,
China
L. Demasi, San Diego State University, San
Diego, CA; R. Gordnier, Air Force Research
NY; Y. Liu, Arizona State University,
Tempe, AZ; A. Saxena, J. Celaya, K.
Goebel, NASA Ames Research Center,
Moffett Field, CA
Y. Xue, AlphaSTAR Corporation, Long
Beach, CA; T. Li, Queensland University of
Technology, Brisbane, Australia; F. Abdi,
AlphaSTAR Corporation, Long Beach, CA
1130 hrs
AIAA-2013-1653
Fatigue Damage Initiation Life
Prediction for Heterogeneous
Metals
1130 hrs
AIAA-2013-1648
Effect of Structural Anisotropy and
Geometric Nonlinearity on Forward
Flapping Wing Flight
Characterization and Estimation of Fatigue Life II
H. Taha, A. Nayfeh, M. Hajj, Virginia
Blacksburg, VA
1100 hrs
AIAA-2013-1647
Exploitation of the Saturation
Phenomenon for Actuation of a
Flapping MAV in Hovering and
Forward Flight
MAVs and Flapping Wings I
Chaired by: K. SHIVAKUMAR, North Carolina Agricultural and Technical State University and A. KELKAR, Joint School of Nanoscience & Nanoengineering
1000 hrs
1030 hrs
1100 hrs
0930 hrs
AIAA-2013-1650
AIAA-2013-1651
AIAA-2013-1652
AIAA-2013-1649
Numerical analysis of fatigue
A time-based formulation for real- Fatigue Damage Diagnosis and
A Probabilistic Framework for Low
behaviors under variable amplitude time fatigue damage prognosis
Prognosis Using Bayesian Updating
Cycle Fatigue Life Prediction and
under variable amplitude loadings T. Peng, Arizona State University, Tempe,
Uncertainty Modeling of Turbine Disk loading
Z. Lu, J. Xu, Beijing Aeronautical Science W. Zhang, Y. Liu, Arizona State University, AZ; J. He, Clarkson University, Potsdam,
Alloys
59-SDM-31
R. Malhan, University of Maryland, College
Park, College Park, MD; P. Masarati,
Technical University of Milan, Milan,
Italy; J. Baeder, I. Chopra, University of
Maryland, College Park, College Park, MD
1100 hrs
AIAA-2013-1643
Mechanics-Based Explanation of
the Second Frequency Branch of
Timoshenko Beam Theory
Beam Dynamics II
Aircraft Gust II
A. Dixit, D. Hodges, Georgia Institute of
Renewable Energy Laboratory, Golden, CO Technology, Atlanta, GA
Chaired by: D. COWAN, Northrop Grumman Corporation and K. HALL, Duke University
0930 hrs
1000 hrs
1030 hrs
AIAA-2013-1644
AIAA-2013-1645
AIAA-2013-1646
CFD-CSD Coupled Aeroelastic
Reduced Order Model for Unsteady Optimization of the Kinematics of
Analysis Of Flexible Flapping Wings Aerodynamics of Flapping Wing
a Flapping Wing MAV in Hover for
For MAV Applications
Micro Air Vehicle in Hover
Enhanced Performance
58-SDM-30
Y. Wang, D. Inman, University of
Chaired by: H. KIM, The Boeing Company and B. WILLIS, The Boeing Company
0930 hrs
1000 hrs
1030 hrs
AIAA-2013-1640
AIAA-2013-1641
AIAA-2013-1642
Experimental and Finite Element Complex Modes in Damped
A Legendre Spectral Finite Element
Analysis for a Multifunctional
Sandwich Beams Using Beam and Implementation of Geometrically
Beam with Frequency-dependent Elasticity Theories
Exact Beam Theory
N. Ahmad, R. Kapania, Virginia Polytechnic
Q. Wang, M. Sprague, National
Viscoelastic Behavior
57-SDM-29
Y. Babbar, V. Suryakumar, T. Strganac,
D. Raveh, Technion--Israel Institute of
Texas A&M University, College Station, TX Technology, Haifa, Israel
Chaired by: Y. MATSUZAKI, Nagoya University and T. KINNEY, NASA-Kenndey Space Center
0930 hrs
1000 hrs
1030 hrs
AIAA-2013-1637
AIAA-2013-1638
AIAA-2013-1639
Aerodynamic Gust Response in
Propagation of Structural Uncertainty
Experiments in Aeroelastic
to Worst Case Gust Loads Predictions
Response and Control under Gust High Angles of Attack
56-SDM-28
Charles River
Imperial Ballroom
Beacon Hill
Cambridge
31
W. Leser, NASA Langley Research Center,
Hampton, VA; F. Yuan, North Carolina State
University, Raleigh, NC; J. Newman, NASA
Langley Research Center, Hampton, VA
WY
Digital Twin II and Multiscale Modeling of Damage in Composites I
Adaptive Structures Conference (ASC) Keynote
62-ASC-4
1300 - 1400 hrs
M. Obenchain, K. Nadella, C. Cesnik,
Arbor, MI
1600 hrs
AIAA-2013-1661
Tensile Testing and Non-destructive
Evaluation Scanning of Varied Ply
CFRP Laminates with Embedded
X. Guan, Siemens Corporation, Princeton, Magnetostrictive Particles
1530 hrs
AIAA-2013-1660
Experimental Identification of
Delamination Size and Location
Based on Signal Correlations
NJ; D. Samaratunga, R. Wang, Clarkson O. Myers, G. Currie, J. Rudd, Mississippi
D. Samaratunga, Clarkson University,
Potsdam, NY; X. Guan, Siemens Corporation, University, Potsdam, NY; R. Jha,
State University, Mississippi State, MS
Mississippi State University, Starkville, MS
Princeton, NJ; R. Jha, Mississippi State
University, Starkville, MS; G. Srinivasan, Indian
Institute of Science, Bangalore, India
Chaired by: V. GIURGIUTIU and A. GHOSHAL, Army Research Laboratory
1430 hrs
1500 hrs
AIAA-2013-1658
AIAA-2013-1659
Hybrid Global Matrix/Local
Wavelet spectral finite element
Interaction Simulation Approach for method for modeling wave
Wave Propagation Simulation in
propagation in stiffened composite
Composite Laminates
laminates
65-ASC-5
Structural Health Monitoring III
Tuesday Afternoon Speakers’ Briefing
64-SB-4
1400 - 1430 hrs
Session Chairs and Speakers in Tuesday Afternoon sessions will meet in their assigned session room.
Tuesday Afternoon Networking Coffee Break
63-BRK-4
1400 - 1430 hrs
Game Changing Activities in the Area of Lightweight Materials and Structures
Stephen W. Gaddis
Program Manager, Org A3 Game Changing Development Program Office, NASA Langley Research Center, Hampton, VA
Tuesday Lunch Break
E. Fang, M. Stuebner, J. Lua, Global
Engineering and Materials, Inc., Princeton,
NJ
61-LNCH-2
1200 - 1300 hrs
San Antonio, TX; J. Ocampo, University of
Texas, San Antonio, San Antonio, TX; K.
Robinson, Southwest Research Institute, San
Antonio, TX
Chaired by: S. WANTHAL, The Boeing Company; G. SEIDEL, Virginia Polytechnic Institute and State Universit; D. STARGEL, AF Office of Scientific Research and E. GLAESSGEN, NASA Langley Research Center
0930 hrs
1000 hrs
1030 hrs
1100 hrs
AIAA-2013-1654
AIAA-2013-1655
AIAA-2013-1656
AIAA-2013-1657
Band-limited Green’s Functions
Random Fiber Micromechanics of X-FEM Co-Simulation of
Investigation of Magnetostrictive
Delamination and Matrix Cracking
Sensor Capabilities for Crack Growth for the Quantitative Evaluation of Fatigue Damage
in Fiber Metal Laminated Structures
Prediction in Second-Layer Structure Acoustic Emission using the Finite M. Garnich, R. Fertig, E. Anderson,
University of Wyoming, Laramie, Laramie, under Fatigue Loading
L. Domyancic, Southwest Research Institute, Element Method
60-SDM-32
Statler
In Session Rooms
Plaza Ballroom
Imperial Ballroom
Lunch on Own
Clarendon
32
A. Crowell, B. Miller, J. McNamara, Ohio
State University, Columbus, OH
T. Murphey, Air Force Research Laboratory,
Kirtland AFB, NM; M. Peterson, M.
Grigoriev, University of New Mexico,
Albuquerque, Albuquerque, NM
M. Muir, EADS, Bristol, United Kingdom; E.
Kolb, A. Parkinson, G. Robertson, C. Muldal,
O. Querin, R. Hewson, V. Toropov, University
of Leeds, Leeds, United Kingdom
A. Jennings, J. Black, Air Force Institute
of Technology, Wright-Patterson AFB,
OH; A. Gutierrez, Trinity University, San
Antonio, TX
1530 hrs
AIAA-2013-1669
Geometry and Moments of Bent
Tape Springs
Beach, CA; S. Liguore, The Boeing
Company, St. Louis, MO
Cambridge, United Kingdom; P.
P. Tagade, H. Choi, Korea Advanced
Constantine, Stanford University, Stanford, Institute of Science and Technology,
CA; P. Gonnet, Durham University, Durham, Daejeon, South Korea
United Kingdom; G. Parks, University of
Cambridge, Cambridge, United Kingdom
M. McEachen, ATK, Goleta, CA
1600 hrs
AIAA-2013-1670
Verification of Deployment
Precision and Stability
Requirements for the GEMS
Telescope Optical Boom
Air Force Research Laboratory, Kirtland
AFB, NM; J. Costantine, California State
University, Fullerton, CA
J. Chaussee, F. Dervault, Bombardier
Aerospace, Saint Laurent, Canada
1630 hrs
AIAA-2013-1678
Knowledge Based Approach
to Wing Weight and Stiffness
Estimation at Early Stages of
Aircraft Design
P. Tagade, H. Choi, Korea Advanced
Institute of Science and Technology,
Daejeon, South Korea
E. DeCarlo, S. Mahadevan, Vanderbilt
University, Nashville, TN; B. Smarslok,
1600 hrs
AIAA-2013-1683
Bayesian Calibration of
Aerothermal Models for Hypersonic
Air Vehicles
C. Fischer, J. Deaton, R. Grandhi, Wright
State University, Dayton, OH
C. Parson, J. Chrissis, R. O’Hara,
A. Palazotto, Air Force Institute of
Technology, Wright-Patterson AFB, OH
1700 hrs
AIAA-2013-1679
Direct Search Optimization of a
Flapping Micro Air Vehicle Wing
1630 hrs
AIAA-2013-1936
Effectiveness of Different ModelForm Quantification Techniques as
Applied to Thermal Physics-Based
Simulations
Non-Deterministic Methods for Aerospace Applications
T. Zill, P. Ciampa, B. Nagel, German
Aerospace Center (DLR), Hamburg,
Germany
1600 hrs
AIAA-2013-1677
A Collaborative MDO Approach for
the Flexible Aircraft
P. Mallol, G. Tibert, Royal Institute of
Technology (KTH), Stockholm, Sweden
1700 hrs
AIAA-2013-1672
Deployment Modeling and
Experimental Testing of a BiG. Olson, S. Pellegrino, California Institute stable Composite Boom for Small
of Technology, Pasadena, CA; J. Banik,
Satellites
1630 hrs
AIAA-2013-1671
Deployable helical antennas for
cubesats
Aerodynamic and Aircraft Optimization
A. Ceruti, University of Bologna, Bologna,
Italy; V. Voloshin, University of Hertfordshire,
Hatfield, United Kingdom; P. Marzocca,
Clarkson University, Potsdam, NY
Chaired by: M. RUMPFKEIL, University of Dayton and T. TORNG, Boeing Defense, Space & Security
1500 hrs
1530 hrs
1430 hrs
AIAA-2013-1681
AIAA-2013-1682
AIAA-2013-1680
Calibration of Computer Simulator Dynamically Bi-orthogonal Field
Sparse Robust Rational
with Non-Gaussian Prior using
Equations for Solution of TwoInterpolation for ParameterDynamically Bi-orthogonal Field
Dimensional Hyperbolic Partial
dependent Aerospace Models
P. Seshadri, University of Cambridge,
Equations
Differential Equations
69-NDA-5
B. Miller, A. Crowell, J. McNamara, Ohio
State University, Columbus, OH
1630 hrs
AIAA-2013-1666
Loosely Coupled Time-Marching
of Fluid-Thermal-Structural
Interactions
Flexible Composites: Hinges and Booms
Chaired by: C. MATTSON, Brigham Young University and L. LURATI, The Boeing Company
1430 hrs
1500 hrs
1530 hrs
AIAA-2013-1674
AIAA-2013-1675
AIAA-2013-1676
Optimization of Aerodynamic
The Use of MDO and Advanced
Multi-Disciplinary Design
Performance and Stability of a
Manufacturing to Demonstrate
Optimization of Unconventional
Stealth Aircraft
Rapid, Agile Construction of a Mission Airship Configurations with Heuristic
H. Taha, M. Hajj, Virginia Polytechnic Institute Optimized UAV
Algorithms
68-MDO-5
M. Peterson, T. Murphey, Air Force
Research Laboratory, Kirtland AFB, NM
Chaired by: S. BRADFORD, Jet Propulsion Laboratory and H. FANG
1430 hrs
1500 hrs
AIAA-2013-1667
AIAA-2013-1668
Large Deformation Bending of Thin Four Point Bending of Thin
Composite Tape Spring Laminates Unidirectional Composite Laminas
67-GSF-4
C. Ostoich, D. Bodony, P. Geubelle, University
of Illinois, Urbana-Champaign, Urbana, IL
D. Pitt, S. Liguore, M. Thomas, N.
Gurtowski, The Boeing Company, St.
Louis, MO
1600 hrs
AIAA-2013-1665
Thermal Acoustic Test and Analysis
Model Updating and Correlation
Multidisciplinary Analysis for Combined Environment Structures II
Chaired by: S. SURAMPUDI, US Air Force and J. SLATER, Wright State University
1430 hrs
1500 hrs
1530 hrs
AIAA-2013-1662
AIAA-2013-1663
AIAA-2013-1664
Robust Treatment of Temperature Verification Studies on Hypersonic
Aerothermoelastic response of a
panel under a high speed turbulent Feedback in Aerothermodynamic Structure Thermal/Acoustic Response
boundary layer using direct numerical Models for Fluid-Thermal-Structural and Life Prediction Methods
G. Tzong, The Boeing Company, Seal
simulation
Analysis
66-DSC-4
Winthrop
Cabot
M. Santer, Imperial College London,
London, United Kingdom
Thoreau
1730 hrs
AIAA-2013-1673
Deployable CubeSat Truss
Structures with Compliant Shape
Memory Hinges
Lexington
33
M. Sunny, S. Mulani, S. Sanyal, R. Pant,
R. Kapania, Virginia Polytechnic Institute
TX; C. Potter, V. Kim, P. Witte, Z. Liu, D.
Mavris, Georgia Institute of Technology,
Atlanta, GA
Company, Niskayuna, NY; M. Tooley,
ANSYS Canada, Ltd., Waterloo, Canada
C. Grappasonni, G. Coppotelli, University
of Rome “La Sapienza”, Rome, Italy;
T. Arsenault, A. Achuthan, P. Marzocca,
Clarkson University, Potsdam, NY
H. Bae, Wright State University, Dayton,
OH; H. Ando, S. Nam, S. Kim, C. Ha,
Caterpillar, Inc., Peoria, IL
1600 hrs
AIAA-2013-1691
Sensor (monitoring points) layout
method for fatigue design load
extraction
Structural Design I
M. Michaeli, Bar-Ilan University, Ramat Gan,
Israel; A. Shtark, H. Grosbein, Israel Military
Industries, Ramat Hasharon, Israel; E. Altus,
Technion--Israel Institute of Technology, Haifa,
Israel; H. Hilton, University of Illinois, UrbanaChampaign, Urbana, IL
N. Myrent, J. Kusnick, D. Adams,
Purdue University, West Lafayette, IN;
D. Griffith, Sandia National Laboratories,
Albuquerque, NM
1630 hrs
AIAA-2013-1697
Geometric Nonlinear Analysis of
Composite Beams using WienerMilenković Parameters
Q. Wang, National Renewable Energy
Laboratory, Golden, CO; W. Yu, Utah
J. Carr, P. Pingle, P. Avitabile, C. Niezrecki, State University, Logan, UT; M. Sprague,
National Renewable Energy Laboratory,
University of Massachusetts, Lowell,
Golden, CO
Lowell, MA
1600 hrs
AIAA-2013-1696
Alternate Techniques/New
Approaches for Identification of
Full Field Dynamic Stress Strain
from Limited Sets of Measured
Data for Wind Turbine Applications
A. Abdelkefi, Y. Zhimiao, M. Hajj, Virginia
Blacksburg, VA
1700 hrs
AIAA-2013-1698
Power Generation from Gallopingbased Piezoaeroelastic Energy
Harvesters for Different CrossSection Geometries
1630 hrs
AIAA-2013-1692
A Unified Approach to
Characterizations of Isotropic Linear
Viscoelastic Moduli and Compliances
without Use of Poisson’S Ratios
Directly from 1-D Tensile Experiments
Wind Turbine Structural Dynamics and Aeroelasticity
Chaired by: J. MCNAMARA, The Ohio State University and C. NIEZRECKI, University of Massachusetts Lowell
1500 hrs
1530 hrs
1430 hrs
AIAA-2013-1694
AIAA-2013-1695
AIAA-2013-1693
High Fidelity Fluid-Structure
On-Condition Evaluation of
Pitch Error and Shear Web Disbond
Interaction Analysis of a Wind
How Inertial and Aerodynamic
Detection on Wind Turbine Blades
Turbine Blade
Characteristics Affect the Dynamics for Offshore Structural Health and
M. Braaten, C. Seeley, General Electric
of a Small Wind Turbine System
Prognostics Management
72-SDM-35
Hampton, VA
Chaired by: B. WILLIS, The Boeing Company and L. HARDAWAY, Ball Aerospace & Technologies Corp
1430 hrs
1500 hrs
1530 hrs
AIAA-2013-1688
AIAA-2013-1689
AIAA-2013-1690
Conceptual Design and Structural An Artificial Neural Network
Development of an Integrated
Analysis of an Open Rotor Hybrid Residual Kriging Based Surrogate Structural Analysis Capability for
Wing Body Aircraft
Model for Shape and Size
Airframe Preliminary Design
F. Gern, NASA Langley Research Center,
Optimization of a Stiffened Panel S. Russell, Triumph Group, Inc., Dallas,
71-SDM-34
J. Weigand, G. Goodmiller, S. TerMaath,
University of Tennessee, Knoxville,
Knoxville, TN
1600 hrs
AIAA-2013-1687
Multi-Scale Investigation of
Composite Aircraft Parts with
Holes to Evaluate the Sensitivity of
Structural Behavior Relative to OutT. Riddle, P. Donnelly, D. Cairns, J. Nelson, of-Plane Laminate Properties
Chaired by: T. OCHINERO, Structural Mechanics Corporation and M. WOLFF, Gulfstream Aerospace Corporation
1430 hrs
1500 hrs
1530 hrs
AIAA-2013-1684
AIAA-2013-1685
AIAA-2013-1686
Use of Statistical Learning in
Structural Reliability Analysis of the Finite Element Analysis of
a Reliability Program for Risk
Advanced Composite Cargo Aircraft Composite Bridge Deck Joints
B. Flansburg, S. Engelstad, Lockheed
N. Sivaneri, West Virginia University,
Assessment of Composite Structures
Martin Corporation, Marietta, GA
Morgantown, WV
With Defects
70-SDM-33
Berkley
Cambridge
St. James
34
E. Carrera, E. Zappino, Technical University M. Karpel, Technion--Israel Institute of
of Turin, Turin, Italy
Technology, Haifa, Israel; A. Shousetrman,
Israeli CFD Center, Cesaria, Israel; H. Climent,
C. Maderuelo, Airbus, Getafe, Spain; A. de la
Serna, Altran, Madrid, Spain
Blacksburg, VA
1530 hrs
AIAA-2013-1702
Dynamic Aeroservoelastic Response
with Nonlinear Structural Elements
H. Ryu, H. Cho, W. Eun, S. Shin, Seoul
National University, Seoul, South Korea;
J. Lee, K. Yee, Pusan National University,
Pusan, South Korea
S. Ghoman, D. Sarhaddi, Z. Wang, P.
Chen, ZONA Technology, Inc., Scottsdale,
AZ
Center, Hampton, VA
Institute, San Antonio, TX; M. Thomsen,
U.S. Air Force, Hill AFB, UT
Chaired by: E. ALTHOF, Raytheon Missile Systems and G. HONEA, Raytheon Missile Systems
1500 hrs
1530 hrs
1430 hrs
AIAA-2013-1717
AIAA-2013-1718
AIAA-2013-1716
Design Improvements and
ModelCenter-Integrated Reduced Hybrid Wing Body Pressurized
Order Multi-fidelity Optimization Fuselage and Bulkhead Design and Analytical Validation for the A-10
Optimization
Wing Replacement Program (WRP)
Scheme for NASA MDAO
V. Mukhopadhyay, NASA Langley Research P. Clark, R. Heller, Southwest Research
Framework
76-SDM-39
F. Nitzsche, D. Feszty, Carleton University, Austin, Austin, TX
Ottawa, Canada; S. Vamosi, Smart Rotor
Systems, Ottawa, Canada
Chaired by: I. CHOPRA, University of Maryland and Y. YANG, Northwestern Polytechnical University
1430 hrs
1500 hrs
1530 hrs
AIAA-2013-1711
AIAA-2013-1712
AIAA-2013-1713
Whirl-tower Open-loop Experiments Investigation of the divergence
Helicopter Forward Flight Prediction
and Simulations with an Adaptive stability boundary of an extremely using Geometrically Exact Beam
Pitch Link Device for Helicopter
flexible helicopter rotor in hover Model and an Advanced Unsteady
J. Sicard, J. Sirohi, University of Texas,
Rotor Vibration Control
Aerodynamics
75-SDM-38
M. Benedict, D. Coleman, D. Mayo, I.
Chopra, University of Maryland, College
I. Mukherjee, S. Sundaram, Indian
Institute of Science, Bangalore, India
F. Sebastiano, S. Ricci, Technical University
of Milan, Milan, Italy
1630 hrs
AIAA-2013-1704
High order harmonic balance
applied to an aeroelastic T-tail
model with a control surface
freeplay
R. Vos, M. Hoogreef, Delft University of
Technology, Delft, The Netherlands
1600 hrs
AIAA-2013-1719
Semi-Analytical Weight Estimation
Method for Fuselages with Oval
Cross-Section
Design: Advanced Aircraft
H. Kang, Army Research Laboratory,
Aberdeen Proving Ground, MD
1600 hrs
AIAA-2013-1714
Elastomeric Damper Models for
Rotorcraft Comprehensive Analysis
Rotorcraft Applications
C. Potter, Georgia Institute of Technology,
Atlanta, GA; S. Russell, Triumph Group, Inc.,
Dallas, TX; V. Kim, P. Witte, Z. Liu, D. Mavris,
Georgia Institute of Technology, Atlanta, GA
of Technology, Delft, The Netherlands;
M. Friswell, W. Dettmer, C. Beaverstock,
Swansea University, Swansea, United
Kingdom
1700 hrs
AIAA-2013-1721
A Preliminary Study of Wing
Substructure Layouts Using a
N. Werter, R. De Breuker, Delft University Parametric Structures Evaluation Tool
1630 hrs
AIAA-2013-1720
Two-level Conceptual Design of
Morphing Wings
M. Riazi, F. Afagh, Carleton University,
Ottawa, Canada
1630 hrs
AIAA-2013-1715
Blade Sailing Phenomenon
Modeling for Feedback Control
1630 hrs
AIAA-2013-1710
Structural and Aerodynamic
Modeling of a Flapping Wing
A. Jennings, Air Force Institute of Technology, Structure
1600 hrs
AIAA-2013-1709
Periodic and Average Flapping
Wing Force Measurement
MAVs and Flapping Wings II
D. Robertson, University of Dayton,
Dayton, OH; G. Reich, Air Force Research
1600 hrs
AIAA-2013-1703
3-D Vortex Particle Aerodynamic
Modelling and Trajectory
Optimization of Perching
Manoeuvres
Computational Aeroservoelasticity
Wright-Patterson AFB, OH; A. Sharp, Virginia
Military Institute, Lexington, VA; D. Doyle,
AFB, OH; A. Sharp, J. Blandino, J. Lysher, J. Black, Air Force Institute of Technology,
Virginia Military Institute, Lexington, VA
Chaired by: D. COWAN, Northrop Grumman Corporation and K. HALL, Duke University
1430 hrs
1500 hrs
1530 hrs
AIAA-2013-1706
AIAA-2013-1707
AIAA-2013-1708
Force and Flowfield Measurements Aerodynamic-Dynamic Interaction Validation of a Finite Element
on a Rigid Wing Undergoing Hover- and Longitudinal Stability of
Analysis of a Flapping Wing against
Capable Flapping and Pitching
Hovering MAVs/Insects
Inertial and Aeroelastic Responses
H. Taha, M. Hajj, A. Nayfeh, Virginia
J. Mason, J. Black, A. Jennings, Air Force
Kinematics in Air at MAV-Scale
Polytechnic Institute and State University, Institute of Technology, Wright-Patterson
Reynolds Numbers
74-SDM-37
W. Anderson, J. Babish, C. Hedgecock,
D. Layton, Lockheed Martin Corporation,
Marietta, GA
Chaired by: R. TOWNER, Jacobs Technology and R. LIND, University of Florida
1430 hrs
1500 hrs
AIAA-2013-1701
AIAA-2013-1699
Full Aircraft Dynamic Response by
A Robust ASE Correlation and
Simplified Structural Models
Analysis Method
73-SDM-36
K. Zeng, J. Xiang, Beihang University,
Beijing, China
Charles River
White Hill
Clarendon
1730 hrs
AIAA-2013-1722
Effects of Nonuniform Elastic
Fuselage Modeling on Flight
Dynamics of Hypersonic Vehicles
Beacon Hill
35
R. Li, S. Steiner, P. Florin, B. Wardle,
Massachusetts Institute of Technology,
Cambridge, MA
P. Prabhakar, A. Waas, University of
Seal Beach, CA; A. Przekop, NASA Langley A. Przekop, Analytical Mechanics Associates,
Inc., Hampton, VA; D. Jegley, NASA Langley
Hampton, VA; A. Lovejoy, D. Jegley, NASA
Langley Research Center, Hampton, VA; B.
Neal, The Boeing Company, Berkeley, MO;
K. Linton, The Boeing Company, Seal Beach,
CA; A. Bergan, J. Bakuckas, Federal Aviation
Administration, Atlantic City, NJ
Chaired by: D. JEGLEY, NASA Langley Research Center and A. VELICKI, The Boeing Company
1500 hrs
1530 hrs
1430 hrs
AIAA-2013-1735
AIAA-2013-1736
AIAA-2013-1734
Analysis of a Hybrid Wing Body
Testing and Analysis Validation of a Nonlinear Analysis and Post-Test
Center Section Test Article
Metallic Repair Applied to a PRSEUS Correlation for a Curved PRSEUS Panel
H. Wu, P. Shaw, The Boeing Company,
K. Gould, Analytical Mechanics Associates, Inc.,
Tension Panel
80-SDM-43
University of Minas Gerais, Belo Horizonte, Technology, Cambridge, MA; S. Kessler,
Brazil
Metis Design Corporation, Boston, MA;
N. Lachmann, J. Gavin, Massachusetts
Institute of Technology, Cambridge, MA;
G. Thomas, Metis Design Corporation,
Boston, MA; B. Wardle, Massachusetts
Chaired by: B. WARDLE, Massachusettes Institute of Technology; J. KOO, The University of Texas at Austin
1430 hrs
1500 hrs
1530 hrs
AIAA-2013-1728
AIAA-2013-1729
AIAA-2013-1730
Nano-Modified Adhesives by
Electrothermal Icing protection
CNT-grafted Carbon Fibers with
Graphene: The Effect Ageing
of Aerosurfaces Using Conductive Preserved Strength Assessed at
Investigation
Polymer Nanocomposites
the Single Fiber and Unidirectional
A. Silva Neto, D. Cruz, A. Avila, Federal
S. Buschhorn, Massachusetts Institute of Composite Scales
78-SDM-41
Wyoming, Laramie, Laramie, WY
1700 hrs
AIAA-2013-1733
Understanding the Influence of
Nickel Doping in a Tungsten Grain
Boundary on Mechanical Strength
1630 hrs
AIAA-2013-1738
Behavior of Frame-Stiffened
Composite Panels with Damage
A. Akepati, N. Hayes, S. Roy, University of H. Lee, V. Tomar, Purdue University, West
Alabama, Tuscaloosa, Tuscaloosa, AL
Lafayette, IN
1630 hrs
AIAA-2013-1732
Multi-scale Modeling of Debond
Behavior in Nano-Particle
Reinforced Polymers
W. Ji, A. Waas, University of Michigan,
A. Lovejoy, NASA Langley Research Center, D. Jegley, NASA Langley Research Center,
Hampton, VA; S. Poplawski, University of Hampton, VA
1600 hrs
AIAA-2013-1737
Preliminary Design and Analysis of
an In-plane PRSEUS Joint
Stitched Unitized Structures
A. Chaurasia, G. Seidel, Virginia
Blacksburg, VA
1600 hrs
AIAA-2013-1731
Computational micromechanics
analysis of electron hopping
induced piezoresistive response
in carbon nanotube-polymer
nanocomposites
Nanostructured Materials II
T. Ricks, T. Lacy, Mississippi State
University, Mississippi State, MS; E.
Pineda, B. Bednarcyk, S. Arnold, NASA
Glenn Research Center, Cleveland, OH
1630 hrs
AIAA-2013-1727
A Predictive Model for the
Compressive Strength of 3D Woven
Textile Composites
Multiscale Modeling of Damage in Composites II
Chaired by: S. WANTHAL, The Boeing Company; G. SEIDEL, Virginia Polytechnic Institute and State Universit and J. RANSOM, NASA Langley Research Center
1430 hrs
1500 hrs
1530 hrs
1600 hrs
AIAA-2013-1723
AIAA-2013-1724
AIAA-2013-1725
AIAA-2013-1726
Failure Mode Predictions in
Modeling fiber-matrix splitting
The Effect of Scale Dependent
On the Use of Volume Average
failure through a mesh-objective Discretization on the Progressive
Constituent Stresses for Predicting the Compressive Response of
Laminated Composites
continuum-decohesive finite
Failure of Composite Materials
Composite Failure
K. Malusare, R. Fertig, University of
P. Prabhakar, A. Waas, University of
element method
Using Multiscale Analyses
77-SDM-40
Constitution
Imperial Ballroom
Stuart
36
Nashville, TN; J. Juang, National Cheng
Kung University, Tainan, Taiwan
H. Monner, T. Haase, M. Misol, S.
Algermissen, German Aerospace Center
(DLR), Braunschweig, Germany
Center, Edwards, CA; D. Mavris, Georgia
Institute of Technology, Atlanta, GA
K. Park, University of Colorado, Boulder,
Boulder, CO; I. Oh, Korea Advanced
Institute of Science and Technology,
Daejeon, South Korea
1100 hrs
AIAA-2013-1742
A gyro-feedback concept for
tailoring the dynamic performance
of metamaterial-based adaptive
systems
Active Control of Structures
S. Bland, R. Snyder, J. Kudva, NextGen
Aeronautics, Inc., Torrance, CA; M. Pontecorvo,
S. Barbarino, F. Gandhi, Rensselaer Polytechnic
Institute, Troy, NY; E. White, The Boeing
Company, Berkeley, MO
1130 hrs
AIAA-2013-1743
Hexagonal Cellular Structures with
Bi-stable Inclined Walls for Energy
Dissipation
Wednesday Morning Networking Coffee Break
Launch Vehicle and Spacecraft Structural Dynamics: State of the Art and Challenges for the Future
Alvar M. Kabe
Associate Principal Director, Structural Mechanics Subdivision, The Aerospace Corporation, El Segundo, CA
Dynamic Specialist Conference (DSC) Keynote
Magnetostrictive Alloys: The Other Smart Material
Alison Flatau
Associate Dean for Research, Clark School of Engineering, University of Maryland, College Park, MD
Chaired by: H. MONNER, DLR - German Aerospace Center and R. BARRETT-GONZALEZ, University of Kansas
0930 hrs
1000 hrs
1030 hrs
AIAA-2013-1739
AIAA-2013-1740
AIAA-2013-1741
Generalized Predictive Control for Feedforward and feedback control Modal Filtering for Control of
Aircraft with Structural Damage
of double panel partition with
Flexible Aircraft
J. Lew, Tennessee State University,
P. Suh, NASA Dryden Flight Research
active trim panel
86-ASC-6
85-BRK-5
0900 - 0930 hrs
84-DSC-5
0800 - 0900 hrs
83-ASME-1
0800 - 0900 hrs
ASME Keynote
Wednesday Morning Speakers’ Briefing
82-SB-5
0730 - 0800 hrs
Session Chairs and Speakers in Wednesday Morning sessions will meet in their assigned session room.
Wednesday Networking Coffee and Pastries
81-NB-3
0700 - 0800 hrs
Wednesday
Statler
Plaza Ballroom
Imperial Ballroom
Georgian Ballroom
In Session Rooms
Plaza Ballroom
37
Z. Riley, J. McNamara, Ohio State
University, Columbus, OH
A. Chaudhuri, University of Florida,
Gainesville, Gainesville, FL; R. Le Riche,
École Nationale Supérieure des Mines de
Saint-Étienne, Saint-Étienne, France; M.
Meunier, Snecma, Villaroche, France
T. Eason, S. Spottswood, Air Force
AFB, OH
1100 hrs
AIAA-2013-1757
Surrogate-based Maximisation of
Belief Function for Robust Design
Optimisation
Composites: Analytical Methods II
1100 hrs
AIAA-2013-1761
Residual Strength of Composite
Laminates with a Hole by Using
Peridynamic Theory
90-SDM-44
Chaired by: I. RAJU, NASA Langley Research Center and M. CHIERICHETTI, Worcester Polytechnic Institute
1000 hrs
1030 hrs
0930 hrs
AIAA-2013-1759
AIAA-2013-1760
AIAA-2013-1758
Comparison Between Different
Strain Energy Method to Model
Development and Validation of
Cellular Cores and Finite Element Composite Structures Damping
a Structural Model for Textile
C. Bisagni, E. Catapano, Technical
Modeling Techniques
Composite Materials
C. Bisagni, M. Pigazzini, Technical
University of Milan, Milan, Italy
H. Soliman, R. Kapania, Virginia
Blacksburg, VA
University of Milan, Milan, Italy
K. Colavito, A. Barut, E. Madenci,
University of Arizona, Tucson, Tucson, AZ;
N. Phan, Naval Air Systems Command,
Patuxent River, MD
Z. Wang, A. Almaktoom, P. Wang, Wichita S. Alicino, M. Vasile, University of
State University, Wichita, KS
Strathclyde, Glasgow, United Kingdom
Optimization Under Uncertainty I
E. Acar, R. Usta, TOBB University of
M. Rumpfkeil, University of Dayton,
Economics and Technology, Ankara, Turkey Dayton, OH
1130 hrs
AIAA-2013-1752
A Model for Quantifying System
Evolvability Based on Excess and
Modularity
Y. Guo, A. Nagy, Z. Gurdal, Delft University
of Technology, Delft, The Netherlands
1130 hrs
AIAA-2013-1762
Modelling of Composite Laminates
Based on Isogeometric Layerwise
Theory
S. Chowdhury, A. Mehmani, J. Zhang, A. M. Tackett, C. Mattson, Brigham Young
Messac, Syracuse University, Syracuse, NY University, Provo, UT; S. Ferguson, North
Carolina State University, Raleigh, NC
1100 hrs
AIAA-2013-1751
Quantifying Regional Error
in Surrogates by Modeling its
Relationship with Sample Density
Optimization Methods
Chaired by: M. RAIS-ROHANI, Mississippi State University and G. SINGH, General Electric - Global Research
0930 hrs
1000 hrs
1030 hrs
AIAA-2013-1753
AIAA-2013-1754
AIAA-2013-1755
Simultaneous Design of a Stiffened Optimization Under Mixed
Dynamic Reliability-Based
Fuselage Panel and Number of
Aleatory/Epistemic Uncertainty
Robust Design with Time-Variant
Structural Tests
Using Derivatives
Probabilistic Constraints
T. Kipouros, University of Cambridge,
Cambridge, United Kingdom; A. Inselberg,
Tel Aviv University, Tel Aviv, Israel; G. Parks,
University of Cambridge, Cambridge, United
Kingdom; A. Savill, Cranfield University,
Cranfield, United Kingdom
1030 hrs
AIAA-2013-1750
Parallel Coordinates in Computational
Engineering Design
ATA Engineering, Inc., San Diego, CA
89-NDA-6
B. Hancock, C. Mattson, Brigham Young
University, Provo, UT
Chaired by: L. WANG and M. RUMPFKEIL, University of Dayton
0930 hrs
1000 hrs
AIAA-2013-1748
AIAA-2013-1749
The Smart Normal Constraint
Estimating Feasibility Using
Method for Directly Generating a Multiple Surrogates and ROC
Smart Pareto Set
Curves
88-MDO-6
R. Deshmukh, J. McNamara, Ohio State
University, Columbus, OH; A. Culler,
1100 hrs
AIAA-2013-1747
A Structures Perspective on
the Challenges Associated with
Analyzing a Reusable Hypersonic
E. Blades, P. Shah, M. Nucci, S. Miskovish, Platform
Multidisciplinary Analysis for Combined Environment Structures III
Chaired by: F. NITZSCHE, Carleton University and K. GRIFFIN, Southwest Research Institute
0930 hrs
1000 hrs
1030 hrs
AIAA-2013-1744
AIAA-2013-1745
AIAA-2013-1746
Assessing Hypersonic Boundary
Demonstration of Multiphysics
Response of Skin Panels to
Combined Self and Boundary Layer Layer Stability in the Presence of Analysis Tools on Representative
Panel Scale Protuberances
Hypersonic Vehicle Structures
Induced Fluctuating Pressure
87-DSC-6
St. James
Winthrop
Cabot
Lexington
38
M. Yekani Fard, S. Sadat, A. Chattopadhyay,
Arizona State University, Tempe, AZ; B. Raji,
Pipe Reconstruction, Phoenix, AZ
P. Naghipour, E. Pineda, B. Bednarcyk,
S. Arnold, NASA Glenn Research Center,
Cleveland, OH
Ahrens, Lockheed Martin Corporation,
Fort Worth, TX; R. Biggs, Lockheed
Martin Corporation, New Orleans, LA;
K. Griffin, Southwest Research Institute,
San Antonio, TX; E. Pendleton, Air Force
AFB, OH
D. Ehrhardt, University of Wisconsin,
Madison, Madison, WI; T. Beberniss,
D. Kumar, C. Cesnik, University of
R. Zhang, Z. Wu, C. Yang, Beihang
University, Beijing, China
Chaired by: J. BLACK, Air Force Institute of Technology and P. PAI, University of Missouri
0930 hrs
1000 hrs
1030 hrs
AIAA-2013-1776
AIAA-2013-1777
AIAA-2013-1779
Ground Structural Coupling Testing Ground Vibration Testing of
and Data Processing Methods for Future responsive Access to Space Dynamic out of Plane Displacement
Frequency Response Function
Airframe Ground Experiment
Error in 3D Digital Image
P. Zink, B. Clark, E. Salcedo, C. Le, J.
Estimation
Correlation
94-SDM-48
K. Ni, Advanced Dynamics, Inc., Lexington, KY E. Muir, P. Friedmann, University of
1030 hrs
AIAA-2013-1774
New Hybrid Optimization for
Design of Active Twist Rotors
1030 hrs
AIAA-2013-1770
A New Theoretical Framework for the
Formulation of General, Nonlinear,
Single-Scale Shell Theories
Langley Research Center, Hampton, VA; H.
T. Williams, Los Alamos National
Kim, University of Bath, Bath, United Kingdom Laboratory, Los Alamos, NM
Chaired by: B. WILLIS, The Boeing Company and P. CENTO, AEDC
0930 hrs
1000 hrs
AIAA-2013-1772
AIAA-2013-1773
Blade Stress Estimation During
Unsteady Aerodynamic Analysis of
Multiple Vibratory Modes
a Bird-Damaged Turbofan
93-SDM-47
X. Ning, S. Pellegrino, California Institute
of Technology, Pasadena, CA
Chaired by: M. SCHULTZ, NASA Langley Research Center and L. DEMASI
1000 hrs
0930 hrs
AIAA-2013-1769
AIAA-2013-1768
Design and testing of imperfection- Structural Assessment of an Advanced
insensitive monocoque cylindrical Composite Tow-Steered Shell
K. Wu, G. Hrinda, Z. Wang, R. Martin, NASA
shells
92-SDM-46
Nashville, TN; S. Clay, Air Force Research
Laboratory, Wright-Patterson AFB, OH; C.
Oskay, Vanderbilt University, Nashville, TN
Chaired by: B. BEDNARCYK, NASA Glenn Research Center and M. SENSMEIER, Embry-Riddle Aeronautical University
0930 hrs
1000 hrs
1030 hrs
AIAA-2013-1763
AIAA-2013-1764
AIAA-2013-1765
Microscale Modelling of FiberModeling Rate Dependent Damage Study of Surface and Sub-surface
Evolution in Composite Structures Damage Initiation and Propagation in Matrix Debonding of SiC/Ti-15-3
M. Bogdanor, R. Crouch, Vanderbilt University, Carbon Epoxy Composites
Laminates under Cyclic Loading
91-SDM-45
Vibration Testing I
J. Beck, J. Brown, Air Force Research
Laboratory, Wright-Patterson AFB,
OH; J. Slater, Wright State University,
Dayton, OH; C. Cross, Air Force Research
1100 hrs
AIAA-2013-1775
Component Mode Reduced Order
Models for Geometric Mistuning of
Integrally Bladed Rotors
Turbomachinery
L. Friedrich, H. Reimerdes, RWTH Aachen
University, Aachen, Germany
S. Gururaja, Indian Institute of Science,
Bangalore, India; M. Ansari, Atkins Global
Consulting, Bangalore, India
1130 hrs
AIAA-2013-1767
Delamination Modeling in Noodle
Region of Composite T-Joints
1100 hrs
AIAA-2013-1771
Imperfection Sensitivity of Circular
Cylindrical Shells of Varying Length
Subjected to Axial Compression
Shells
W. McLendon, J. Whitcomb, Texas A&M
1100 hrs
AIAA-2013-1766
Progressive Failure of Plain Weave
Textiles Under Multiaxial Loading
Composites: Damage Evolution
Beacon Hill
Clarendon
Charles River
Cambridge
39
University, Blacksburg, VA; N. Lindsley,
Institute of Technology, Harbin, China
K. Knipe, D. Siljee, A. Manero, S. Raghavan,
University of Central Florida, Orlando, FL;
J. Okasinski, J. Almer, Argonne National
Laboratory, Argonne, IL; S. Rangaswamy,
Intelligent Automation, Inc., Rockville, MD
Multifunctional Materials I
H. Su, M. Ryan, Ohio State University,
Canada; J. Garnand-Royo, Virginia
Columbus, OH
Blacksburg, VA; A. Suleman, University of
Victoria, Victoria, Canada; R. Canfield, C.
Woolsey, Virginia Polytechnic Institute and
State University, Blacksburg, VA
Panelists:
Julie Christodoulou
Office of Naval Research
98-SDM-52
0930 - 1200 hrs
N. Yamamoto, E. Gdoutos, C. Daraio,
California Institute of Technology,
Pasadena, CA
S. Soghrati, A. Najafi, N. Sottos, S. White,
P. Geubelle, University of Illinois, UrbanaChampaign, Urbana, IL
Greg Olson
QuesTek Innovations
Northwestern University
David Furrer
Pratt & Whitney
1130 hrs
AIAA-2013-1793
Computational Design of ActivelyCooled Microvascular Composite
Skin Panels for Hypersonic Aircraft
D. Robertson, University of Dayton,
Dayton, OH; G. Reich, Air Force Research
1130 hrs
AIAA-2013-1788
Design and Perching Experiments
of Bird-like Remote Controlled
Planes
Dale Ball
Lockheed Martin Corporation
Integrated Computational Material Engineering and the Materials Genome Initiative
Chaired by: K. SHIVAKUMAR, North Carolina Agricultural and Technical State University and A. KELKAR, Joint School of Nanoscience & Nanoengineering
1000 hrs
1030 hrs
1100 hrs
0930 hrs
AIAA-2013-1790
AIAA-2013-1791
AIAA-2013-1792
AIAA-2013-1789
Engineered thin films with ultra-low Electromechanical stability and
Simulations Mapping Stress
Modeling of Residual Stresses in
thermal expansion coefficient for dynamic analysis of dielectric
Evolution in High Temperature
Shape Memory Alloy - Ceramic
deployable or deformable space
elastomer plane actuators
Ceramic Coatings under Thermal- Composites
L. Liu, J. Leng, J. Chen, Y. Liu, Harbin
B. Lester, D. Lagoudas, Texas A&M
structures
Mechanical Conditions
97-SDM-51
V. Hrishikeshavan, C. Bogdanowicz, I.
Chopra, University of Maryland, College
1100 hrs
AIAA-2013-1787
Peak Input Torque Minimization
of a Flapping Wing Mechanism
for MAVs
H. Hu, National Cheng Kung University, Tainan,
Taiwan; W. Lin, Chinese Military Academy,
Fengshan, Taiwan; L. Ke, National Cheng Kung
University, Tainan, Taiwan
Design: Micro/Unmanned Aircraft
Chaired by: C. DAUWALTER, Milli Sensor Systems and Actuators Inc and L. SAAM, ATA Engineering, Inc. (HQ)
0930 hrs
1000 hrs
1030 hrs
AIAA-2013-1784
AIAA-2013-1785
AIAA-2013-1786
Nonlinear Aeroelastic Scaled Model Design and Evaluation of
Performance of a Wing-Propeller Optimization Using Equivalent
Aeroelastically Tuned Joined-Wing
System for a Quad-Rotor-Biplane Static Loads
SensorCraft Flight Test Article
A. Ricciardi, R. Canfield, M. Patil, C. Eger, J. Richards, University of Victoria, Victoria,
Micro Air Vehicle
M. Jrad, M. Sunny, R. Kapania, Virginia
Blacksburg, VA
96-SDM-50
Aberdeen Proving Ground, MD; A. Waas, L. Borkowski, A. Chattopadhyay, Arizona
University of Michigan, Ann Arbor,
State University, Tempe, AZ
Ann Arbor, MI; C. Yen, Army Research
Laboratory, Aberdeen Proving Ground, MD
1100 hrs
AIAA-2013-1783
Nonlinear Analysis of Fiber-Reinforced
Composite Laminates Subjected to
Uniaxial Compressive Load
Characterization and Modeling of Composite Laminates
Chaired by: D. POWELL, Southern Research Institute and A. AVILA, Universidade Federal de Minas Gerais
0930 hrs
1000 hrs
1030 hrs
AIAA-2013-1780
AIAA-2013-1781
AIAA-2013-1782
Ab Initio Micromechanics Based
Global-local analysis of a composite
Through-the-thickness response of
hybrid 2D and 3D woven composites Multiscale Model of Woven Ceramic plate with a rectangular notch of a
M. Pankow, Army Research Laboratory,
Matrix Composites
large aspect ratio
95-SDM-49
Franklin
Stuart
Constitution
Merle Giles
National Center for Supercomputing Applications
University of Illinois
Berkley
40
J. Dias, C. De Marqui, University of São Paulo, T. Silva, C. De Marqui, University of São
São Carlos, Brazil; A. Erturk, Georgia Institute Paulo, São Carlos, Brazil
of Technology, Atlanta, GA
Hampton, VA
Research Agency (FOI), Stockholm, Sweden; P. Acar, M. Nikbay, Istanbul Technical
J. Heeg, P. Chwalowski, NASA Langley
University, Istanbul, Turkey
Chaired by: P. TAYLOR, Gulfstream Aerospace Corporation and E. BLADES, ATA Engineering, Inc.
1500 hrs
1530 hrs
1430 hrs
AIAA-2013-1799
AIAA-2013-1800
AIAA-2013-1798
Initial Investigation of the Benchmark Steady and Unsteady Aeroelastic
Overview and Lessons Learned
SuperCritical Wing Configuration using Computations of HIRENASD
from the Aeroelastic Prediction
Hybrid RANS-LES modeling
Wing for Low and High Reynolds
Workshop
J. Heeg, NASA Langley Research Center, M. Dalenbring, A. Jirasek, Swedish Defense Numbers
103-DSC-7
Rensselaer Polytechnic Institute, Troy, NY
Chaired by: I. CHOPRA, University of Maryland and O. MYERS, Mississippi State University
1500 hrs
1530 hrs
1430 hrs
AIAA-2013-1795
AIAA-2013-1796
AIAA-2013-1794
Dimensionless analysis and scaling
Vibration Suppression of a PlateEnergy Dissipation of a Bi-stable
of a hybrid 3DOF airfoil-based
Like Wing Under Atmospheric
von-Mises Truss under Impulsive
piezoelectric-inductive aeroelastic
Turbulence Using Passive And
Excitation
S. Barbarino, M. Pontecorvo, F. Gandhi,
energy harvester
Hybrid Piezoelectric Circuits
102-ASC-7
C. Wieseman, NASA Langley Research
Center, Hampton, VA
1600 hrs
AIAA-2013-1801
Structural Dynamics Modeling
of HIRENASD in support of the
Aeroelastic Prediction Workshop
J. Heeg, D. Piatak, NASA Langley Research
Center, Hampton, VA
1630 hrs
AIAA-2013-1802
Experimental data from the
Benchmark SuperCritical Wing
wind tunnel test on an oscillating
turntable
The Aeroelastic Prediction Workshop
S. Barbarino, M. Pontecorvo, F. Gandhi,
Rensselaer Polytechnic Institute, Troy, NY;
S. Bland, R. Snyder, J. Kudva, NextGen
Aeronautics, Inc., Torrance, CA; E. White,
The Boeing Company, Berkeley, MO
1600 hrs
AIAA-2013-1797
A Novel Structural Element
Combining Load Carrying and
Energy Dissipation Capability
Modeling and Analysis I
Wednesday Afternoon Speakers’ Briefing
101-SB-6
1400 - 1430 hrs
Session Chairs and Speakers in Wednesday Afternoon sessions will meet in their assigned session room.
Wednesday Afternoon Networking Coffee Break
Computational Models in the Materials World: We Are Nearly There…
David Furrer
Senior Fellow Discipline Lead, Pratt & Whitney, East Hartford, CT (with Rollie Dutton, Air Force Research Laboratory, Wright-Patterson AFB, OH)
100-BRK-6
1400 - 1430 hrs
99-LNCH-3
1200 - 1400 hrs
Lexington
Franklin
In Session Rooms
Plaza Ballroom
Imperial Ballroom
41
Pini, Technical University of Milan, Milan,
Italy
G. Corriveau, F. Dervault, Bombardier
Aerospace, Saint Laurent, Canada
University, Nashville, TN
O. Stohlman, J. Fernandez, V. Lappas,
University of Surrey, Guildford, United
Kingdom; M. Hillebrandt, C. Hühne, M.
Straubel, German Aerospace Center (DLR),
Braunschweig, Germany
1630 hrs
AIAA-2013-1807
Testing of the Deorbitsail drag sail
subsystem
M. Rouhi, M. Rais-Rohani, Mississippi
State University, Mississippi State, MS
1630 hrs
AIAA-2013-1812
Effect of Nano-inclusions on
Probabilistic Design of Components
Made of Hybrid Composite
Materials
1600 hrs
AIAA-2013-1816
Adaptive Importance Sampling for
Optimization under Uncertainty
Using Stochastic Simulation
Optimization Under Uncertainty II
C. Eacker, M. Riley, University of Idaho,
Moscow, Moscow, ID
1600 hrs
AIAA-2013-1811
Optimization of Computational
Laminate Composites for the
Prediction of Performance Metrics
Using Finite Element Simulation
J. Medina, A. Taflanidis, University of
P. Seshadri, G. Parks, University of Cambridge, Notre Dame, Notre Dame, IN
Cambridge, United Kingdom; S. Shahpar,
Rolls-Royce Group plc, Derby, United Kingdom
Chaired by: R. GRANDHI, Wright State University and L. LURATI, The Boeing Company
1500 hrs
1530 hrs
1430 hrs
AIAA-2013-1814
AIAA-2013-1815
AIAA-2013-1813
Inclusion of Data Uncertainty and Hybrid Adjoint-based Robust
Robust Design of a Transonic
Model Error in Multi-disciplinary
Optimization Approach for Fluid- Axial Compressor Blade Using a
Analysis and Optimization
Dynamics Problems
Hybrid Optimization-Uncertainty
C. Liang, S. Mahadevan, Vanderbilt
P. Cinnella, DynFluid, Paris, France; M.
Quantification Approach
106-NDA-7
S. Mulani, Virginia Polytechnic Institute
D. Walch, S. Tetreault, F. Dervault,
and State University, Blacksburg, VA; D. Bombardier Aerospace, Montréal, Canada
Havens, Lockheed Martin Corporation,
Marietta, GA; A. Norris, Lockheed Martin
Corporation, Palmdale, CA; R. Bird, NASA
Langley Research Center, Hampton, VA; R.
Kapania, Virginia Polytechnic Institute and
State University, Blacksburg, VA; R. Olliffe,
Lockheed Martin Corporation, Marietta, GA
1530 hrs
AIAA-2013-1810
Impact of Wing Box Geometrical
Parameters on Stick Model
Prediction Accuracy
O. Stohlman, V. Lappas, University of
Surrey, Guildford, United Kingdom
1600 hrs
AIAA-2013-1806
Deorbitsail: a deployable sail for
de-orbiting
Solar Sails and Drag De-Orbiters
Composite and Structural Optimization I
1530 hrs
AIAA-2013-1805
DEPLOYTECH : nano-satellite
testbeds for gossamer technologies
A. Viquerat, M. Schenk, V. Lappas,
University of Surrey, Guildford, United
H. Sakamoto, S. Kadonishi, Y. Satou, H.
Furuya, Tokyo Institute of Technology, Tokyo, Kingdom
Japan; Y. Shirasawa, N. Okuizumi, O. Mori, H.
Sawada, Japan Aerospace Exploration Agency
(JAXA), Kanagawa, Japan; J. Matsumoto,
University of Tokyo, Tokyo, Japan; M. Natori,
Waseda University, Tokyo, Japan; Y. Miyazaki,
Nihon University, Chiba, Japan; M. Okuma,
Tokyo Institute of Technology, Tokyo, Japan
1500 hrs
AIAA-2013-1804
Repeatability of Stored
Configuration of a Large Solar Sail
with Non-negligible Thickness
Chaired by: R. CANFIELD, Virginia Tech and J. MARTINS, University of Michigan
1430 hrs
1500 hrs
AIAA-2013-1808
AIAA-2013-1809
Design, Optimization, and
Smeared Stiffeners in Panel for
Evaluation of Al-2139 Compression Mesh Simplification at Conceptual
Panel with Integral T-Stiffeners
Design Phase
105-MDO-7
G. Greschik, TentGuild Engineering
Company, Boulder, CO
Chaired by: N. BARNES, L’Garde, Inc
1430 hrs
AIAA-2013-1803
A Linear Photonic Thrust Model and
its Application to the L’Garde Solar
Sail Surface
104-GSF-6
Winthrop
Cabot
Thoreau
42
T. Matsumura, R. Haftka, N. Kim,
University of Florida, Gainesville,
Gainesville, FL
H. Hilton, S. D’Urso, University of Illinois,
Urbana-Champaign, Urbana, IL
Bristol, Bristol, United Kingdom
C. Park, N. Kim, R. Haftka, University of
Florida, Gainesville, Gainesville, FL
1530 hrs
AIAA-2013-1819
The effect of the number of
coupon and element tests on
conservativeness
Pennsylvania State University, University
Park, PA
Southampton, Southampton, United Kingdom; A. Shaw, S. Neild, D. Wagg, P. Weaver,
B. LePage, G. Richardson, Surrey Satellite
University of Bristol, Bristol, United
Technology, Ltd., Guildford, United Kingdom Kingdom; A. Carrella, LMS International,
Leuven, Belgium
T. Li, H. Deng, Xidian University, Xi’an,
China; X. Ma, China Academy of Space
Technology, Xi’an, China; J. Jiang, Z. Lin,
Xidian University, Xi’an, China
1630 hrs
AIAA-2013-1829
Design and Analysis of Space
Deployable Antennas Composed of
Scissor-Like Hinges Driven by Springs
D. Wilckens, F. Odermann, A. Kling,
German Aerospace Center (DLR),
Braunschweig, Germany
1630 hrs
AIAA-2013-1824
Buckling and Post Buckling of
Stiffened CFRP Panels under
Compression and Shear - Test and
Numerical Analysis
Damping and Vibration Suppression
Y. Zong, H. Cao, Xidian University, Xi’an,
K. Blunck, T. Coon, E. Swenson, J. Black, China
R. Cobb, Air Force Institute of Technology,
1600 hrs
AIAA-2013-1828
Optimal Pretension Design of
Tension Truss Deployable Reflectors
Based on ATCM
Space Structures
K. Liang, M. Abdalla, Z. Gurdal, Delft
University of Technology, Delft, The
Netherlands
1600 hrs
AIAA-2013-1823
Buckling Imperfection-Sensitivity
Analysis Using a Koiter-Newton
Approach
Joints, Aeroelasticity, and Buckling
Reliability Testing
K. Bender, N. Muturi, A. Spies, C. Lee,
Franklin W. Olin College of Engineering,
Needham, MA
Chaired by: T. BARTKOWICZ, The Boeing Company; J. BLACK, Air Force Institute of Technology and R. MALLA, University of Connecticut
1500 hrs
1530 hrs
1600 hrs
1430 hrs
AIAA-2013-1832
AIAA-2013-1833
AIAA-2013-1834
AIAA-2013-1831
A General Methodology for Analysis of Experimental Investigation Into A Aeroelastic Energy Harvesting
Multi-layered Radial Isolator for
Vibration Isolator Incorporating A Using a Nonlinear Electromagnetic
Helicopter Interior Noise Reduction Structure-Borne Micro-Vibration
P. Autran, D. Materkowski, G. Lesieutre, M. Remedia, W. Aglietti, University of
Bistable Composite Plate
Oscillator
110-SDM-55
T. Johnson, D. Sleight, R. Martin, NASA
Chaired by: J. DOMBER, Ball Aerospace & Technologies Corp and J. HEALD, Canadian Space Agnecy
1430 hrs
1500 hrs
1530 hrs
AIAA-2013-1825
AIAA-2013-1826
AIAA-2013-1827
Structures and Design Phase
Substrate Prototype Development Space Telescope Structural
I Summary for the NASA
for Tensioned Phased Arrays
Design Analysis for the
J. Mejia-Ariza, L’Garde, Inc., Tustin, CA
Composite Cryotank Technology
Chromotomographic Hyperspectral
Demonstration Project
Imaging Experiment
109-SDM-54
Center (DLR), Hamburg, Germany
Chaired by: T. KRISHNAMURTHY, NASA-Langley Research Center and R. KOCH, Naval Undersea Warfare Center
1430 hrs
1500 hrs
1530 hrs
AIAA-2013-1820
AIAA-2013-1821
AIAA-2013-1822
A Hierarchical Aeroelastic Engine
Designer Euler and Elastica
Postbuckling Response of Variable
for the Preliminary Design and
Columns Subjected to Aerodynamic
Angle Tow Composite Plates Under
Optimization of the Flexible Aircraft Loads - System Engineering of the
Shear Load
P. Ciampa, T. Zill, B. Nagel, German Aerospace Aeroelasticity of Wind Turbine Towers G. Raju, Z. Wu, P. Weaver, University of
108-SDM-53
C. Quintana, H. Millwater, University of
Texas, San Antonio, San Antonio, TX; R.
Penmetsa, Air Force Research Laboratory,
Chaired by: S. ADHIKARI, Swansea University
1430 hrs
1500 hrs
AIAA-2013-1817
AIAA-2013-1818
Conservativeness in Failure
Investigating the Feasibility of
Probability Estimate: Redesign Risk
Interpolating Scatter in Material
vs. Performance
Property Data
107-NDA-8
F. Zheng, Xidian University, Xi’an, China
1700 hrs
AIAA-2013-1830
Deploying Ability Analyses of a
Folded Hoop-Rib Space Deployable
Structure
Beacon Hill
Clarendon
Cambridge
St. James
43
Japan
D. Sleight, R. Martin, T. Johnson, NASA
Naval Research, Arlington, VA
D. Handlin, H. Cebeci, M. Williams,
E. Parsons, S. Socrate, B. Wardle,
Massachusetts Institute of Technology,
Cambridge, MA
1600 hrs
AIAA-2013-1850
The Coming ICME Data Tsunami
and What Can be Done
H. Huang, Universal Technology
J. Estevez, M. Ghazizadeh, A. Kelkar,
Corporation, Dayton, OH; A. Roy, Air Force Joint School of Nanoscience and
Nanoengineering, Greensboro, NC
AFB, OH; S. Sihn, University of Dayton
Research Institute, Dayton, OH
Worth, TX
J. Choi, S. Yang, M. Cho, Seoul National
University, Seoul, South Korea
1600 hrs
AIAA-2013-1857
Exceptional interfacial properties of
structurally defected CNT/polymer
nanocomposites: a molecular
dynamics study
Nanostructured Materials III
OH; T. Wong, Pratt & Whitney, Canoga
Park, CA
M. Enright, J. McFarland, R. McClung,
Southwest Research Institute, San Antonio,
TX; W. Wu, R. Shankar, Scientific Forming
Technologies Corporation, Columbus, OH
S. Luo, W. Obitayo, T. Liu, Florida State
University, Tallahassee, FL
1630 hrs
AIAA-2013-1859
SWCNT Thin Film Enabled
Piezoresistive Fiber Sensors Fabrication, Characterization and
Application for SHM of Polymeric
1630 hrs
AIAA-2013-1851
Probabilistic Integration of Material
Process Modeling and Fracture Risk
S. Arnold, F. Holland, T. Gabb, M. Nathal, Assessment Using Gaussian Process
D. Ball, Lockheed Martin Corporation, Fort NASA Glenn Research Center, Cleveland, Models
Chaired by: B. WARDLE, Massachusettes Institute of Technology and E. GLAESSGEN, NASA Langley Research Center
1500 hrs
1530 hrs
1430 hrs
AIAA-2013-1855
AIAA-2013-1856
AIAA-2013-1853
On the studies of coarse-grained
Property Prediction of Single Wall
Three-Dimensional Constitutive
carbon nanotubes as structural
Boron Nitride Nanotubes using MD
Relations of Aligned Carbon
Simulation
Nanotube Polymer Nanocomposites elements
114-SDM-59
Evanston, IL
R. Scigliano, R. Gardi, A. Del Vecchio,
Italian Aerospace Research Center (CIRA),
Capua, Italy
P. Richards, P. Mardanpour, R. Herd, D.
Hodges, Georgia Institute of Technology,
Atlanta, GA
1600 hrs
AIAA-2013-1846
Thermo-structural design of Ultra
High Temperature Ceramic (UHTC)
winglets of a re-entry space vehicle
Design: Spacecraft II
J. Rothkegel, G. Dimitriadis, University of
Liège, Liège, Belgium
1630 hrs
AIAA-2013-1840
The Effect of Inertial and
Constitutive Properties on BodyFreedom Flutter of a Flying Wing
Integrated Computational Materials Engineering (ICME)
S. Pendleton, J. Basile, J. Shepard, B.
Fowler, Moog-CSA Engineering, Mountain
View, CA
1530 hrs
AIAA-2013-1845
Launch Locked Strut for On-orbit
Isolation Utilizing Viscoelastic
Damping
Chaired by: J. MATLIK, Rolls-Royce Corporation and S. ROY, The University of Alabama
1430 hrs
1500 hrs
1530 hrs
AIAA-2013-1847
AIAA-2013-1848
AIAA-2013-1849
Integrated Computational Materials ICME - Application of the
An Early Demonstration of the Role
Design: From Genome o Flight
Revolution to Titanium Structures that ICME Can Play in Airframe
G. Olson, QuesTek Innovations, LLC,
W. Mullins, J. Christodoulou, Office of
Design and Cost Analyses
113-SDM-58
R. Williams, K. Maxhimer, T. Brennan, L.
Lai, Raytheon Company, El Segundo, CA
Chaired by: J. CUTSHALL and B. ROBBERS, Aerojet
1430 hrs
1500 hrs
AIAA-2013-1843
AIAA-2013-1844
Design of Radar Panel Mounting
Structural Design and Sizing of a
Hardware for ISIS Radar Antenna Metallic Cryotank Concept
112-SDM-57
Technology, Wright-Patterson AFB, OH; N. M. Padmanabhan, Duke University,
Lindsley, Air Force Research Laboratory,
Durham, NC; C. Pasiliao, Air Force
Research Laboratory, Eglin AFB, FL; E.
Dowell, Duke University, Durham, NC
1600 hrs
AIAA-2013-1839
Dynamic Stall and Stall Flutter
Simulations for a 2D Airfoil Using
Viscous-Inviscid Coupling
Limit Cycle Oscillations (LCO) and Aircraft Flutter
Chaired by: B. WILLIS, The Boeing Company and D. PITT, Boeing Engineering Operations & Technology
1430 hrs
1500 hrs
1530 hrs
AIAA-2013-1836
AIAA-2013-1837
AIAA-2013-1838
Flutter Prediction of Multimode
Computation Investigation of the An Approach to Aeroelastic
Effect of Missile Control Surfaces on Modeling and Simulation of Limit Systems from their Turbulent
Cycle Oscillations of Aircraft Wings Responses by Jury’s Criterion
F-16 Limit Cycle Oscillation
C. Hanson, D. Kunz, Air Force Institute of with Stores
Y. Matsuzaki, Nagoya University, Nagoya,
111-SDM-56
A. Achuthan, Clarkson University, Potsdam,
NY; B. Bednarcyk, S. Arnold, NASA Glenn
Research Center, Cleveland, OH
Constitution
Stuart
Charles River
N. Muturi, A. Spies, K. Bender, C. Lee,
Franklin W. Olin College of Engineering,
Needham, MA
1730 hrs
AIAA-2013-1842
Stall Flutter Oscillation
Measurements from a Two Degreeof-Freedom Airfoil with Nonlinear
Stiffness
1700 hrs
AIAA-2013-1852
Efficient Multiscale Plasticity
Model for Polycrystalline Materials
Based on Micromechanical
Homogenization
P. Bansal, The Boeing Company,
Bangalore, India; D. Pitt, The Boeing
Company, St. Louis, MO
1700 hrs
AIAA-2013-1841
Stochastic Variations in
Aerodynamic Influence Coefficients
(AICs) on Flutter Prediction of a
Generic Wing
Berkley
44
Gossamer Systems Forum (GSF) Keynote
University, Durham, NC
M. Morton, T. Lewis, Lockheed Martin
Corporation, Marietta, GA
H. Arizono, Japan Aerospace Exploration
Agency (JAXA), Mitaka, Japan; C. Cesnik, K. Lai, National University of Singapore,
Singapore, Singapore
Arbor, MI
1100 hrs
AIAA-2013-1863
Reduced-Order Aeroelastic
Modeling Using Coupled CFDCSD Simulations and System
Identification Technique
1030 hrs
AIAA-2013-1862
Computational Static Aeroelasticity
Using Nonlinear Structures and
Aerodynamics Models
Computational Aeroelasticity I
Chaired by: K. GRIFFIN, Southwest Research Institute
0930 hrs
1000 hrs
AIAA-2013-1860
AIAA-2013-1861
Discrete Adjoint Method for
Strouhal Frequency Influence on
Nonlinear Aeroelastic Sensitivities the Vibration Specification for
for Compressible and Viscous Flows a Flat Blade Antenna Subject to
J. Thomas, E. Dowell, K. Hall, Duke
Upstream Proturbances
Thursday Morning Networking Coffee Break
The Role of MDO in the Design for Complex Engineered Systems
Christina Bloebaum
Dennis and Rebecca Muilenburg Professor of Aerospace Engineering, Iowa State University, Ames, IA
120-DSC-8
119-BRK-7
0900 - 0930 hrs
118-MDO-8
0800 - 0900 hrs
Multidisciplinary Design Optimization (MDO) Keynote
Thursday Morning Speakers’ Briefing
117-SB-7
0730 - 0800 hrs
Session Chairs and Speakers in Thursday Morning sessions will meet in their assigned session room.
Thursday Networking Coffee and Pastries
116-NB-4
0700 - 0800 hrs
Thursday
SPS-ALPHA: A Practical New Approach to the Vision of the Solar Power Satellite
John Mankins
CEO, Artemis Innovation Management Solutions LLC, Santa Maria, CA
John C. Mankins, CEO of Artemis Innovation Management Solutions LLC, a 25 year veteran of the Jet Propulsion Laboratory (JPL) and an internationally recognized leader in space systems and technology innovation,
will present a practical new approach for harvesting sunlight to provide vast amounts of sustainable energy.
115-GSF-7
1800 - 1900 hrs
Franklin
Plaza Ballroom
Imperial Ballroom
In Session Rooms
Plaza Ballroom
Georgian Ballroom
45
University of Colorado, Boulder, Boulder,
CO
H. Kim, University of Bath, Bath, United
Kingdom; R. Guyer, Los Alamos National
Laboratory, Los Alamos, NM
AFB, OH
J. Mullins, C. Li, S. Sankararaman, S.
Mahadevan, Vanderbilt University, Nashville,
TN; A. Urbina, Sandia National Laboratories,
Albuquerque, NM
Technologies, Inc., Moffett Field, CA;
S. Mahadevan, Vanderbilt University,
Nashville, TN
D. Bergman, B. Yang, University of
Southern California, Los Angeles, CA; H.
Fang, Shanghai Yue-Sheng Technology,
Inc., Shanghai, China
V. Romero, L. Swiler, A. Urbina, Sandia
National Laboratories, Albuquerque, NM; J.
Mullins, Vanderbilt University, Nashville, TN
1100 hrs
AIAA-2013-1875
A Comparison of Methods for
Representing and Aggregating
Uncertainties involving Sparsely
Sampled Random Variables - Final
Results
1130 hrs
AIAA-2013-1868
Curvilinear Quasi-Static Model for
Analysis of Shape Memory Polymer
Composite Cantilever Beams for
Space Applications
Non-Deterministic Model Validation and Calibration
Chaired by: J. PEPIN, Los Alamos National Laboratory and S. VENKATARAMAN, San Diego State University
1000 hrs
1030 hrs
0930 hrs
AIAA-2013-1873
AIAA-2013-1874
AIAA-2013-1872
Probabilistic Integration of Validation Assessing the Reliability of
Challenging issues in Bayesian
and Calibration Results for Prediction Computational Models under
calibration of multi-physics models
Y. Ling, S. Mahadevan, Vanderbilt
Level Uncertainty Quantification:
Uncertainty
University, Nashville, TN
S. Sankararaman, Stinger Ghaffarian
Application to Structural Dynamics
123-NDA-9
University of Lisbon, Lisbon, Portugal
Topology Optimization
J. Fulcher, I. Scherrer, S. Smith, University
of Kentucky, Lexington, Lexington, KY; J.
Baker, University of Kentucky, Paducah,
Paducah, KY
1100 hrs
AIAA-2013-1867
Using Nonlinear FE Modeling to
Understand the Effect of Boundary
Conditions on Precise Surfaces of
Chaired by: H. KIM, University of Bath and V. BALABANOV, Boeing Commercial Airplanes
0930 hrs
1000 hrs
1030 hrs
AIAA-2013-1869
AIAA-2013-1870
AIAA-2013-1871
Topology Optimization of a Wing Robust Topology Optimisation with Aeroelastic Topology Optimization
Including Self-Weight Load
Generalised Probability Distribution of Blade-Stiffened Panels
L. Felix, A. Gomes, A. Suleman, Technical of Loading
B. Stanford, P. Beran, M. Bhatia, Air Force
122-MDO-9
D. Lichodziejewski, Airborne Systems,
Santa Ana, CA; R. Dillman, NASA Langley
Research Center, Hampton, VA; D.
Jurewicz, Airborne Systems, Santa Ana,
CA; K. Johnson, NASA Langley Research
Center, Hampton, VA; A. Cassell, NASA
Ames Research Center, Moffett Field, CA;
B. Tutt, Airborne Systems, Santa Ana, CA
Chaired by: G. GRESCHIK, TentGuild Engineering Co and V. LAPPAS, University of Surrey
0930 hrs
1000 hrs
1030 hrs
AIAA-2013-1864
AIAA-2013-1865
AIAA-2013-1866
Bending Properties of Bellows-Type Remote Charging Mechanics for
Ground and Flight Testing of
Inflatable Tube Elements
Electrostatic Inflation of Membrane
a Stacked Torus Hypersonic
Inflatable Aerodynamic Decelerator H. Furuya, J. Yokoyama, Tokyo Institute of Space Structures
Technology, Yokohama, Japan
L. Stiles, Z. Sternovsky, H. Schaub,
Configuration
121-GSF-8
Winthrop
Cabot
Thoreau
46
Peggy Payne Academy, Tempe, AZ; A.
Chattopadhyay, Arizona State University,
Tempe, AZ; B. Raji, Pipe Reconstruction,
Phoenix, AZ
J. Min, NASA Glenn Research Center,
Cleveland, OH
T. Metlen, A. Palazotto, Air Force Institute Institute of Technology, Harbin, China
of Technology, Wright-Patterson AFB, OH
Storrs, Storrs, CT
J. Choi, Virginia Polytechnic Institute
and State University, Blacksburg, VA; D.
Inman, University of Michigan, Ann Arbor,
Ann Arbor, MI
G. Guruswamy, NASA Ames Research
Center, Moffett Field, CA
1100 hrs
AIAA-2013-1892
Vibration Analysis of StringHarnessed Beam Structures: A
Homogenization Approach
1130 hrs
AIAA-2013-1887
Navier-Stokes based Unsteady
Aerodynamic Computations of
Launch Vehicles undergoing Forced
Coupled Oscillations
String, Cable, and Wiring Dynamics
B. Lenahen, S. Gangadharan, M. Desai,
Embry-Riddle Aeronautical University,
Daytona Beach, FL
1100 hrs
AIAA-2013-1886
A Computational and Experimental
Analysis of Spacecraft Propellant
Tanks Implemented with Flexible
Diaphragms
K. Spak, Virginia Polytechnic Institute and J. Kauffman, University of Central Florida, B. Martin, A. Salehian, University of
State University, Blacksburg, VA; G. Agnes, Orlando, FL; G. Lesieutre, Pennsylvania
Waterloo, Waterloo, Canada
Jet Propulsion Laboratory, California
State University, University Park, PA
Institute of Technology, Pasadena, CA; D.
Inman, University of Michigan, Ann Arbor,
Ann Arbor, MI
Chaired by: V. BABUSKA, Sandia National Laboratories and Y. YIU, Lockheed Martin Corporation
1000 hrs
1030 hrs
0930 hrs
AIAA-2013-1889
AIAA-2013-1890
AIAA-2013-1888
Towards Modeling of CableDamping Models for Timoshenko
Development of predictive
Harnessed Structures: Cable
Beams with Applications to
modeling for Cable Harnessed
Damping Experiments
Spacecraft Wiring Harnesses
Structure
127-SDM-63
J. Noël, G. Kerschen, University of Liège,
Liège, Belgium
Space and Launch Vehicle Structural Dynamics
Chaired by: G. GURUSWAMY, NASA-Ames and B. COYNE, United Launch Alliance
0930 hrs
1000 hrs
1030 hrs
AIAA-2013-1883
AIAA-2013-1884
AIAA-2013-1885
Nonparametric Subspace
Ambient Vibration Testing of a
Dynamic and Contact Analysis of a
Identification of Nonlinear
Segmented Mirror Telescope
Special Percussive Mechanism for
A. Jennings, R. Cobb, Air Force Institute of Planetary Subsurface Exploration
Structures - Application to a
Technology, Wright-Patterson AFB, OH
L. Vila, R. Malla, University of Connecticut,
Spacecraft
126-SDM-62
University, Cranfield, United Kingdom
Structural Design II
P. Parkes, R. Butler, D. Almond, University
of Bath, Bath, United Kingdom
1100 hrs
AIAA-2013-1879
Fatigue of Metal-Composite Joints
with Penetrative Reinforcement
Composites: Fatigue and Fracture II
Chaired by: L. DOMYANCIC, Southwest Research Institue and D. COPE, Southwest Research Institue
0930 hrs
1000 hrs
1030 hrs
AIAA-2013-1880
AIAA-2013-1881
AIAA-2013-1882
Optimal Design and Analysis of a
Design of a Structure that Achieves A Novel Lattice-Based Design and
Wing with Morphing High Lift Devices Positive Buoyancy in Air Using a
Analysis of Inflatable Wing
S. Guo, S. Ahmed, N. Di Matteo, Cranfield Vacuum
C. Wang, Y. Liu, L. Zhang, P. Gong, Harbin
125-SDM-61
Chaired by: V. RANATUNGA, Miami Univeristy and O. ZHUPANSKA, The University of Iowa
0930 hrs
1000 hrs
1030 hrs
AIAA-2013-1876
AIAA-2013-1877
AIAA-2013-1878
Study of Fatigue and Post-Fatigue
Micromechanics Fatigue Damage
Crack Arrestment of Bonded
Behavior of Stitch-bonded Composites Analysis Modeling for Fabric
Composite Joints
J. Action, S. Engelstad, Lockheed Martin M. Yekani Fard, S. Sadat, Arizona State
Reinforced Ceramic Matrix
Corporation, Marietta, GA
University, Tempe, AZ; E. Postelnicu,
Composites
124-SDM-60
Clarendon
Beacon Hill
Cambridge
Lexington
47
H. Hesse, R. Palacios, Imperial College
P. Pai, D. Feng, Y. Duan, University of
Missouri, Columbia, Columbia, MO
Processes in Aerospace Materials
131-SDM-67
North Carolina A&T State University,
Greensboro, NC
H. Shin, S. Chang, S. Yang, M. Cho, Seoul State University, Tempe, AZ
National University, Seoul, South Korea
Chaired by: D. POWELL, Southern Research Institute and M. JACINTO, Pratt & Whitney
1000 hrs
1030 hrs
0930 hrs
AIAA-2013-1905
AIAA-2013-1906
AIAA-2013-1903
Stochastic multiscale analysis
Flexural Over-strength Factor for
Interleaved Polymer Matrix
considering the uncertainties in MD Epoxy Resin Materials
Composites - A Review
K. Shivakumar, R. Panduranga, M. Sharpe, simulation and manufacture
M. Yekani Fard, A. Chattopadhyay, Arizona
M. Yekani Fard, S. Sadat, A. Chattopadhyay,
Arizona State University, Tempe, AZ; B. Raji,
Pipe Reconstruction, Phoenix, AZ
1100 hrs
AIAA-2013-1907
Effects of Curing Temperature and
Environmental Conditions on Mode
I Fracture Behavior for a Laminated
Biaxial Carbon/Epoxy Composite
A. Kamal, M. Gresil, V. Giurgiutiu, University of J. Bao, Y. Shen, V. Giurgiutiu, University of
1100 hrs
AIAA-2013-1902
Nonlinear Wave Propagation
Simulation for Lap Joint
Structural Health Monitoring with
Piezoelectric Wafer Active Sensors
Institute, Lianyungang, China
Multifunctional Materials II and Materials for Structural Health Monitoring
Vibration Testing II
Very Flexible Aircraft
Chaired by: W. YU and G. SEIDEL, Virginia Polytechnic Institute and State Universit
0930 hrs
1000 hrs
1030 hrs
AIAA-2013-1899
AIAA-2013-1900
AIAA-2013-1901
Initial Feasibility of Protective Skins Theory and Experiment Research of Comparative Study of Several
for Composite Airliners
Metamaterial Panel for Mechanical Methods for the Calculation
V. Johnson, R. Boone, S. Jones, V. Pendse, Waves Absorption
of Ultrasonic Guided Waves in
Cessna Aircraft Company, Wichita, KS
H. Sun, Jiangsu Automation Research
Composites
130-SDM-66
M. Chierichetti, Worcester Polytechnic Institute, E. Hernandez, K. Erazo, University of
Worcester, MA; C. Grappasonni, G. Coppotelli, Vermont, Burlington, Burlington, VT
University of Rome “La Sapienza”, Rome,
Italy; M. Ruzzene, Georgia Institute of
Technology, Atlanta, GA
Chaired by: Y. CHUNG, The Boeing Company and M. ALLEN, University of Wisconsin
0930 hrs
1000 hrs
1030 hrs
AIAA-2013-1896
AIAA-2013-1897
AIAA-2013-1898
A modal approach for dynamic
Experimental verification of a finite High-Fidelity Camera-based
response monitoring from
element model based functional
Method for Noncontact Vibration
experimental data
observer for structural systems
Testing of Structures
129-SDM-65
Beijing, China
1030 hrs
AIAA-2013-1895
Model Reduction in Flexible-Aircraft
Dynamics with Large Rigid-Body
L. Wang, C. Xie, C. Yang, Beihang University, Z. Wan, C. Cesnik, University of Michigan, Motion
Chaired by: D. RAVEH and S. SURAMPUDI, US Air Force
0930 hrs
1000 hrs
AIAA-2013-1893
AIAA-2013-1894
Static Aeroelastic Analysis of Flexible Geometrically Nonlinear Aeroelastic
Scaling for Very Flexible Aircraft
Aircraft with Large Deformations
128-SDM-64
Statler
Stuart
Berkley
St. James
48
L. Lambert, H. Najafian, University of
Liverpool, Liverpool, United Kingdom;
J. Cooper, University of Bristol, Bristol,
United Kingdom
1430 hrs
AIAA-2013-1922
Navier-Stokes-Based Dynamic
Simulations of Sling Loads
1500 hrs
AIAA-2013-1923
Store Ejection Loads Analysis Using
an Euler Solver
Computational Aeroelasticity II
T. Carpenter, R. Albertani, Oregon State
University, Corvallis, OR
1500 hrs
AIAA-2013-1917
Aerodynamic load estimation:
Pressure distribution from
virtual strain sensors for a pliant
membrane wing
SMA Applications
A. Samur, A. Erturk, Georgia Institute of
1500 hrs
AIAA-2013-1911
Multifunctional double-bimorph
piezoelectric composite for bendingtwisting actuation, adaptive stiffness
change, and energy harvesting
O. Soto, J. Baum, SAIC, McLean, VA; R.
Lohner, George Mason University, Fairfax, VA
V. Malladi, P. Tarazaga, Virginia
Blacksburg, VA
1530 hrs
AIAA-2013-1918
Modeling of Hysteretic Effects of
SMA using Neuro Fuzzy Inference
System
Blacksburg, VA
S. Zhao, A. Erturk, Georgia Institute of
J. Sun, X. Gong, Y. Liu, J. Leng, Harbin
Institute of Technology, Harbin, China
1600 hrs
AIAA-2013-1919
Variable Camber Wing Based on
Shape Memory Polymer Skin
1600 hrs
AIAA-2013-1913
Numerical and experimental
comparison of bistable and
monostable vibration energy
A. Kancharala, M. Philen, Virginia
harvesters under broadband
Polytechnic Institute and State University, random excitation
1530 hrs
AIAA-2013-1912
Application of MFCs for Enhanced
Performance of Flexible Flapping
Fins
Israeli CFD Center, Cesaria, Israel; H.
Climent, M. Reyes, Airbus, Getafe, Spain
1530 hrs
AIAA-2013-1924
Inter-Element Stabilization for Linear
Large-Deformation Elements to Solve
D. Prosser, M. Smith, Georgia Institute of P. Chen, Z. Zhang, ZONA Technology, Inc., Coupled CFD/CSD Blast and Impact
Technology, Haifa, Israel; A. Shousterman, Technology, Atlanta, GA
Scottsdale, AZ
problems
Chaired by: D. GRIFFITH and J. COOPER, University of Bristol
1330 hrs
1400 hrs
AIAA-2013-1920
AIAA-2013-1921
Probabilistic Modelling of Aircraft Dynamic Response to Wake
Response to Non-Gaussian
Encounter
M. Karpel, Technion--Israel Institute of
Continuous Turbulence
136-DSC-9
T. Machairas, University of Patras, Patras,
Greece; D. Hartl, Texas A&M University,
College Station, TX; D. Saravanos, University
of Patras, Patras, Greece; D. Lagoudas, Texas
A&M University, College Station, TX
1430 hrs
AIAA-2013-1916
A Study of Substrate Materials for
Use in Conjunction with Macro Fiber
Composites
C. Seeley, General Electric Company,
Niskayuna, NY
1430 hrs
AIAA-2013-1910
Determination of Hydrofoil
Damping Due to Fluid Structure
Interaction Using MFC Actuators
College Park, College Park, MD; F. Righi, B. LaCroix, P. Ifju, University of Florida,
D. Hartl, J. Rogers, Texas A&M University, Gainesville, Gainesville, FL
College Station, TX
O. Curet, A. Carrere, R. Waldman, K.
Breuer, Brown University, Providence, RI
1400 hrs
AIAA-2013-1909
Aerodynamic Characterization of
Wing Membrane with Adaptive
Compliance
Chaired by: D. SARAVANOS, University of Patras and D. DOYLE, USAF
1400 hrs
1330 hrs
AIAA-2013-1914
AIAA-2013-1915
Multilevel Optimization of a Morphing Shape Memory Alloy Rotor Blade
Deicing
Structure Incorporating Shape
D. Sullivan, University of Maryland,
Memory Alloy Wires
135-ASC-9
B. Woods, M. Friswell, Swansea
University, Swansea, United Kingdom
Chaired by: C. SEELEY and W. YU
1330 hrs
AIAA-2013-1908
Fluid-Structure Interaction Analysis
of the Fish Bone Active Camber
Mechanism
134-ASC-8
Modeling and Analysis II
Thursday Afternoon Speakers’ Briefing
133-SB-8
1300 - 1330 hrs
Session Chairs and Speakers in Thursday afternoon sessions will meet in their assigned session room.
Thursday Lunch Break
132-LNCH-4
1200 - 1300 hrs
Franklin
Cambridge
Statler
In Session Rooms
Lunch on Own
49
M. Thamann, S. Smith, University of
Kentucky, Lexington, Lexington, KY
R. Sandhu, M. Khalil, Carleton University,
Ottawa, Canada; D. Poirel, Royal Military
College of Canada, Kingston, Canada; A.
Sarkar, Carleton University, Ottawa, Canada
D. An, J. Choi, Korea Aerospace University, G. Bartram, S. Mahadevan, Vanderbilt
Goyang, South Korea; N. Kim, University University, Nashville, TN
of Florida, Gainesville, Gainesville, FL
Chaired by: T. KRISHNAMURTHY, NASA-Langley Research Center
1400 hrs
1330 hrs
AIAA-2013-1941
AIAA-2013-1940
Options for Prognostics Methods: A Integrating Heterogeneous
review of data-driven and physics- Information in Diagnosis and
Prognosis
based prognostics
140-NDA-11
M. Riley, University of Idaho, Moscow,
Moscow, ID
Chaired by: J. PEPIN, Los Alamos National Laboratory
1330 hrs
1400 hrs
AIAA-2013-1937
AIAA-2013-1938
Evidence-Based Quantification
Model Selection Methods for
of Model-Form Uncertainties in
Nonlinear Aeroelastic Systems
Simulation-Based Analyses
Using Wind Tunnel Data
139-NDA-10
D. Locatelli, A. Yeilaghi Tamijani, S. Mulani, Q. O. Weckner, V. Balabanov, The Boeing
Liu, R. Kapania, Virginia Polytechnic Institute Company, Seattle, WA
Chaired by: P. ROHL, Advatech Pacific Inc and A. SRIVASTAVA
1330 hrs
1400 hrs
AIAA-2013-1931
AIAA-2013-1932
Multidisciplinary Optimization of
Facesheet stiffness effects in the
Supersonic Wing Structures Using
design of composite sandwich
Curvilinear Spars and Ribs (SpaRibs) structures
138-MDO-10
and State University, Blacksburg, VA;
S. Ashcraft, M. Thamann, S. Smith,
University of Kentucky, Lexington,
Lexington, KY
1530 hrs
AIAA-2013-1935
Optimal Parameter Selection of
an SVM Model: Application to Hip
Fracture Risk Prediction
D. Li, Beihang University, Beijing, China; S. P. Jiang, S. Missoum, University of
Guo, Cranfield University, Bedford, United Arizona, Tucson, Tucson, AZ
Kingdom
1500 hrs
AIAA-2013-1934
Optimization of Composite Wing
Structure for a Flying Wing Aircraft
Subject to Multi Constraints
Y. Wang, P. Wang, Wichita State
University, Wichita, KS
1430 hrs
AIAA-2013-1942
Cost Benefit Analysis of Condition
Monitoring Systems for Optimal
Maintenance Decision Making
C. Wang, L. Lan, Y. Liu, L. Zhang, H. Tan,
Harbin Institute of Technology, Harbin,
China
1600 hrs
AIAA-2013-1930
A Numerical Algorithm for
Eliminating the Singular Stiffness
Matrix of Membrane Wrinkling
1530 hrs
AIAA-2013-1944
A Multi-attribute Classification
Fusion System for Structural Health
Diagnostics
T. Torng, The Boeing Company, Huntington
P. Tamilselvan, P. Wang, Wichita State
Beach, CA; J. Ihn, The Boeing Company,
University, Wichita, KS
Seattle, WA; K. Halbert, The Boeing Company,
Philadelphia, PA; C. Davis, The Boeing
Company, Seattle, WA; L. Fitzwater, The
Boeing Company, Seal Beach, CA
1500 hrs
AIAA-2013-1943
Integration of a Time Varying
Probability of Detection (POD)
Model for Structural Integrity
Non-Deterministic Maintenance, Monitoring and Prognostics
P. Bisaillon, R. Sandhu, M. Khalil, A.
Sarkar, Carleton University, Ottawa,
Canada; D. Poirel, Royal Military College
of Canada, Kingston, Canada
Non-Deterministic Model Error and Selection
D. Cross, R. Canfield, Virginia Polytechnic
1430 hrs
AIAA-2013-1933
Continuum Shape Sensitivity with
Spatial Gradient Reconstruction of
Built-up Structures
1430 hrs
AIAA-2013-1939
Model Selection for Strongly
Nonlinear Systems
K. Woo, Y. Kim, Chungbuk National
University, Cheongju, South Korea; C.
Jenkins, Montana State University,
Bozeman, MT
1530 hrs
AIAA-2013-1929
Ballistic Penetration of Thin
Aluminum Foil
Composite and Structural Optimization II
A. Senba, Nagoya University, Nagoya,
Japan; Y. Ogi, University of Tokyo,
Komaba, Japan; N. Kogiso, Osaka
Prefecture University, Sakai, Japan
1500 hrs
AIAA-2013-1928
Wrinkle/Slack Control Using Shape
Memory Polymer Films for Large
Membrane Structures
Membrane Mechanics and Active Control
K. Senda, M. Petrovic, Kyoto University,
Kyoto, Japan
Chaired by: M. SILVER, MIT Lincoln Laboratory and J. HEALD, Canadian Space Agnecy
1330 hrs
1400 hrs
1430 hrs
AIAA-2013-1925
AIAA-2013-1926
AIAA-2013-1927
Behavior of a Sheared Square
Design of a Rapid Prototype Wing Modeling and Flight Testing of
Wing Shaping for Autonomous
Membrane with Cyclic Boundary
Warping Test Aircraft
E. Doepke, Virginia Polytechnic Institute Flight Control
Conditions during Wrinkling
137-GSF-9
Winthrop
Clarendon
Cabot
Thoreau
50
Blacksburg, VA; A. Nuhait, King Saud
University, Riyadh, Saudi Arabia
C. Teng, W. Yu, Utah State University,
Logan, UT
A. Molavi Tabrizi, E. Pan, University of
Akron, Akron, OH
Logan, UT
H. Kapoor, Virginia Polytechnic Institute
1500 hrs
AIAA-2013-1952
Free Vibration and Linear Dynamics
Analysis of Composite Plate Using
NURBS Isogeometric Finite Element
Analysis
Plate and Cylinder Dynamics
F. Yipaer, C. Sultan, Virginia Polytechnic
Institute and State University, Blacksburg,
VA
C. Lord, J. Rongong, University of
Sheffield, Sheffield, United Kingdom
1530 hrs
AIAA-2013-1953
A Single Layer Constitutive Model
for the Dynamics and Vibration
Damping of Layered Built-up
Structures Using Microslip and
Macroslip Models
1500 hrs
AIAA-2013-1948
Modern Control Design for A
Membrane with Bimorph Actuators
Membrane Structural Dynamics
S. Behdad, B. Boesl, Florida International
University, Miami, FL
1500 hrs
AIAA-2013-1957
Multiscale characterization and
experimentation on particulate
reinforced composites
L. Zhang, W. Yu, Utah State University,
Logan, UT
1530 hrs
AIAA-2013-1958
A Variational Asymptotic Method for
Unit Cell Homogenization of ElastoViscoplastic Heterogeneous Materials
Multiscale Modeling and Characterization of Composites
Chaired by: R. NAIK, Pratt & Whitney and A. AVILA, Universidade Federal de Minas Gerais
1400 hrs
1430 hrs
1330 hrs
AIAA-2013-1955
AIAA-2013-1956
AIAA-2013-1954
Fundamental Solutions of
Homogenization of High Porosity
Micromechanics Modeling of
Heterogeneous Materials with
Transversely Isotropic Trimaterial Materials and Structures Using
Nonuniformly Distributed Loads
Due to Point Forces via Cylindrical Shell Elements
Z. Ye, W. Yu, Utah State University,
System of Vector Functions
and Temperature
143-SDM-70
A. Smith, NASA Marshall Space Flight
F. Fazzolari, J. Banerjee, City University
Center, Huntsville, AL; B. LaVerde, ERC,
Inc., Huntsville, AL; D. Jones, R. Towner,
Jacobs, Huntsville, AL; R. Hunt, Bevilacqua
Research Corporation, Huntsville, AL
Chaired by: C. HEBERT, Sierra Nevada Corporation and J. RISTOW, NASA Kennedy Space Center
1330 hrs
1400 hrs
1430 hrs
AIAA-2013-1949
AIAA-2013-1950
AIAA-2013-1951
A Patch Density Recommendation A Refined Dynamic Stiffness
Effectiveness of Nonlinear Energy
based on Convergence Studies for Element for Free Vibration Analysis Sink (NES) in Suppressing VortexVehicle Panel Vibration Response of Composite Circular Cylindrical
Induced Vibrations of a Circular
resulting from Excitation by a
Shells Based on a Unified
Cylinder
A. Mehmood, M. Hajj, A. Nayfeh, Virginia
Diffuse Acoustic Field
Formulation
142-SDM-69
Boulder, CO; W. Wilkie, NASA Langley
P. Chen, Z. Wang, S. Yang, Z. Zhou, ZONA Tokyo, Japan; A. Kanda, Japan Aerospace
Research Center, Hampton, VA; E. Dowell, Technology, Inc., Scottsdale, AZ
Exploration Agency (JAXA), Tokyo, Japan
Duke University, Durham, NC
Chaired by: D. LICHODZIEJEWSKI, Airborne Systems NA and K. SCHULTZ, NASA Johnson Space Center
1330 hrs
1400 hrs
1430 hrs
AIAA-2013-1945
AIAA-2013-1946
AIAA-2013-1947
Dynamic Aeroelastic Instability
Detection of wrinkles in membrane
Rectangular Solar Sail Flutter
S. Gibbs, Duke University, Durham, NC; D. Investigations on A Wrinkling
structures by elastic wave propagation
Guerrant, University of Colorado, Boulder, Aeroshell/Ballute Configuration
Y. Akaike, T. Yokozeki, University of Tokyo,
141-SDM-68/GSF-10
Stuart
Berkley
Beacon Hill
51
Abbeel, P., 28-MDO-3
Abdalla, M., 108-SDM-53
Abdelkefi, A., 33-SDM-15, 35-SDM-17, 72-SDM-35
Abdi, F., 45-ASC-3, 59-SDM-31
Acar, E., 89-NDA-6
Acar, P., 103-DSC-7
Achuthan, A., 72-SDM-35, 113-SDM-58
Action, J., 124-SDM-60
Adams, D., 72-SDM-35
Adhikari, S., 29-NDA-2, 107-NDA-8
Adomeit, A., 36-SDM-18
Afagh, F., 75-SDM-38
Aglietti, W., 110-SDM-55
Agnes, G., 26-GSF-2, 127-SDM-63
Ahmad, N., 57-SDM-29
Ahmed, S., 125-SDM-61
Ahrens, J., 94-SDM-48
Ajaj, R., 5-ASC-1
Akaike, Y., 141-SDM-68/GSF-10
Akepati, A., 78-SDM-41
Akhavan, H., 34-SDM-16
Albertani, R., 135-ASC-9
Algermissen, S., 86-ASC-6
Alicino, S., 89-NDA-6
Allen, M., 25-DSC-2, 129-SDM-65
Allison, J., 8-MDO-1, 28-MDO-3
Almaktoom, A., 89-NDA-6
Almer, J., 97-SDM-51
Almond, D., 124-SDM-60
Alonso, J., 9-NDA-1
Alpay, S., 11-SDM-2
Altenbuchner, C., 24-ASC-2
Althof, E., 76-SDM-39
Altus, E., 71-SDM-34
Ameri, N., 7-GSF-1
An, D., 140-NDA-11
Anderson, E., 60-SDM-32
Anderson, W., 73-SDM-36
Ando, H., 71-SDM-34
Ansari, M., 91-SDM-45
Ardelean, E., 26-GSF-2
Arizono, H., 120-DSC-8
Arnold, S., 10-SDM-1, 77-SDM-40, 91-SDM-45, 113-SDM-58
Arrieta, A., 24-ASC-2, 27-MDO-2
Arsenault, T., 72-SDM-35
Ashcraft, S., 137-GSF-9
Askari, A., 17-SDM-8
Atcheson, P., 7-GSF-1
Atmeh, G., 53-SDM-25
Atri, M., 50-SDM-22
Attar, P., 29-NDA-2
Autran, P., 110-SDM-55
Avila, A., 78-SDM-41, 95-SDM-49, 143-SDM-70
Avitabile, P., 72-SDM-35
Azevedo, J., 14-SDM-5
Babbar, Y., 56-SDM-28
Babish, J., 73-SDM-36
Babuska, V., 16-SDM-7, 127-SDM-63
Badcock, K., 15-SDM-6
Bae, H., 71-SDM-34
Baeder, J., 58-SDM-30
Baier, H., 26-GSF-2
Bailey, M., 36-SDM-18
Baines, A., 37-SDM-19
Bakeer, B., 16-SDM-7
Baker, J., 121-GSF-8
Bakker, C., 28-MDO-3
Bakuckas, J., 80-SDM-43
Balabanov, V., 122-MDO-9, 138-MDO-10
Ball, D., 113-SDM-58
Banerjee, J., 142-SDM-69
Banik, J., 67-GSF-4
Bansal, P., 111-SDM-56
Bao, J., 130-SDM-66
Barbarino, S., 86-ASC-6, 102-ASC-7
Barnes, N., 104-GSF-6
Barone, M., 32-SDM-14
Barrett-Gonzalez, R., 86-ASC-6
Bartkowicz, T., 110-SDM-55
Bartram, G., 140-NDA-11
Barut, A., 30-SDM-12, 31-SDM-13, 90-SDM-44
Basile, J., 112-SDM-57
Bauchau, O., 50-SDM-22
Baum, J., 136-DSC-9
Beaverstock, C., 76-SDM-39
Beberniss, T., 94-SDM-48
Beck, J., 93-SDM-47
Bednarcyk, B., 10-SDM-1, 77-SDM-40, 91-SDM-45, 113-SDM-58
Behdad, S., 143-SDM-70
Bender, K., 110-SDM-55, 111-SDM-56
Bendiksen, O., 6-DSC-1, 46-DSC-3
Benedict, M., 32-SDM-14, 74-SDM-37
Beran, P., 6-DSC-1, 122-MDO-9
Bergan, A., 80-SDM-43
Bergman, D., 121-GSF-8
Bhachu, K., 8-MDO-1
Bhatia, M., 6-DSC-1, 27-MDO-2, 122-MDO-9
Bichiou, Y., 33-SDM-15
Bichon, B., 9-NDA-1
Biggs, R., 94-SDM-48
Bilgen, O., 24-ASC-2
Bird, R., 105-MDO-7
Bisagni, C., 30-SDM-12, 90-SDM-44
Bisaillon, P., 139-NDA-10
Black, J., 67-GSF-4, 74-SDM-37, 94-SDM-48,
109-SDM-54, 110-SDM-55
Blades, E., 87-DSC-6, 103-DSC-7
Bland, S., 86-ASC-6, 102-ASC-7
Blandino, J., 26-GSF-2, 74-SDM-37
Blunck, K., 109-SDM-54
Bodony, D., 66-DSC-4
Boesl, B., 143-SDM-70
Bogdanor, M., 91-SDM-45
Bogdanowicz, C., 96-SDM-50
Bojanowski, C., 36-SDM-18
Boone, R., 130-SDM-66
Borkowski, L., 95-SDM-49
Braaten, M., 72-SDM-35
Bradford, S., 26-GSF-2, 67-GSF-4
Brennan, N., 45-ASC-3
Brennan, T., 112-SDM-57
Breuer, K., 134-ASC-8
Broughton, B., 18-SDM-9
Brown, A., 17-SDM-8
Brown, J., 93-SDM-47
Bruck, H., 31-SDM-13
Buentello Hernandez, R., 19-SDM-10
Buschhorn, S., 78-SDM-41
Bushnell, D., 12-SDM-3
Butler, R., 124-SDM-60
Cairns, D., 54-SDM-26, 70-SDM-33
Campos, L., 55-SDM-27
Canfield, R., 27-MDO-2, 33-SDM-15, 96-SDM-50, 105-MDO-7, 138-MDO-10
Cao, H., 109-SDM-54
Cardoso, J., 5-ASC-1
Carpenter, T., 135-ASC-9
Carr, J., 72-SDM-35
Carrella, A., 110-SDM-55
Carrera, E., 30-SDM-12, 73-SDM-36
Carrere, A., 134-ASC-8
Cassell, A., 121-GSF-8
Catapano, E., 90-SDM-44
Cater, C., 52-SDM-24
Cavagna, L., 15-SDM-6
Cavallaro, R., 33-SDM-15
Cebeci, H., 114-SDM-59
Celaya, J., 59-SDM-31
Cento, P., 93-SDM-47
Ceruti, A., 68-MDO-5
Cesnik, C., 55-SDM-27, 65-ASC-5, 93-SDM-47,
120-DSC-8, 128-SDM-64
Chakravarty, S., 49-NDA-4
Chan, W., 30-SDM-12
Author/Session Chair Index
Chang, S., 131-SDM-67
Chapman, R., 53-SDM-25
Charmbalis, G., 33-SDM-15
Chattopadhyay, A., 24-ASC-2, 30-SDM-12, 91-SDM-45, 95-SDM-49, 124-SDM-60, 131-SDM-67
Chaudhuri, A., 88-MDO-6
Chaurasia, A., 78-SDM-41
Chaussee, J., 68-MDO-5
Chen, G., 18-SDM-9
Chen, H., 46-DSC-3
Chen, J., 97-SDM-51
Chen, P., 76-SDM-39, 136-DSC-9, 141-SDM-68/GSF-10
Chen, X., 19-SDM-10
Chierichetti, M., 90-SDM-44, 129-SDM-65
Cho, H., 50-SDM-22, 75-SDM-38
Cho, M., 10-SDM-1, 30-SDM-12, 114-SDM-59, 131-SDM-67
Choi, H., 69-NDA-5
Choi, J., 114-SDM-59, 127-SDM-63, 140-NDA-11
Chopra, I., 32-SDM-14, 58-SDM-30, 74-SDM-37, 75-SDM-38, 96-SDM-50, 102-ASC-7
Chowdhury, S., 88-MDO-6
Chrissis, J., 28-MDO-3, 68-MDO-5
Christensen, A., 31-SDM-13
Christodoulou, J., 113-SDM-58
Chung, Y., 129-SDM-65
Chwalowski, P., 103-DSC-7
Ciampa, P., 68-MDO-5, 108-SDM-53
Cinnella, P., 106-NDA-7
Clark, B., 94-SDM-48
Clark, P., 76-SDM-39
Clay, S., 91-SDM-45
Climent, H., 73-SDM-36, 136-DSC-9
Cobb, R., 109-SDM-54, 126-SDM-62
Coimbra, J., 48-MDO-4
Colavito, K., 90-SDM-44
Coleman, D., 74-SDM-37
Colombini, E., 38-SDM-20
Constantine, P., 69-NDA-5
Contreras, M., 36-SDM-18
Cooley, P., 16-SDM-7
Coon, T., 109-SDM-54
Cooper, J., 5-ASC-1, 24-ASC-2, 33-SDM-15,
56-SDM-28, 136-DSC-9
Cope, D., 53-SDM-25, 125-SDM-61
Coppotelli, G., 72-SDM-35, 129-SDM-65
Corriveau, G., 105-MDO-7
Cosmo, M., 53-SDM-25
Costantine, J., 67-GSF-4
Couch, A., 45-ASC-3
Cowan, D., 58-SDM-30, 74-SDM-37
Coyne, B., 126-SDM-62
Crawford, C., 54-SDM-26
Creary, G., 18-SDM-9
Cross, C., 93-SDM-47
Cross, D., 138-MDO-10
Crouch, R., 91-SDM-45
Crowell, A., 66-DSC-4
Cruz, D., 78-SDM-41
Culler, A., 25-DSC-2, 87-DSC-6
Curet, O., 134-ASC-8
Currie, G., 65-ASC-5
Cutler, J., 48-MDO-4
Cutshall, J., 112-SDM-57
D’Urso, S., 108-SDM-53
Da Ronch, A., 15-SDM-6
Da Silva, R., 14-SDM-5
Dafnis, A., 36-SDM-18
Dale, A., 24-ASC-2
Dalenbring, M., 103-DSC-7
Danner, R., 47-GSF-3
Daraio, C., 97-SDM-51
Das, S., 49-NDA-4
Datashvili, L., 26-GSF-2
Dauwalter, C., 96-SDM-50
Davidson, B., 31-SDM-13
Davidson, P., 51-SDM-23
Davis, C., 140-NDA-11
Davis, G., 26-GSF-2
De Breuker, R., 76-SDM-39
de la Serna, A., 73-SDM-36
De Marqui, C., 102-ASC-7
Deaton, J., 8-MDO-1, 69-NDA-5
DeCarlo, E., 69-NDA-5
Del Vecchio, A., 112-SDM-57
Demasi, L., 33-SDM-15, 58-SDM-30, 92-SDM-46
Deng, H., 36-SDM-18, 109-SDM-54
Denhart, J., 48-MDO-4
Dervault, F., 68-MDO-5, 105-MDO-7
Desai, M., 126-SDM-62
Deshmukh, A., 28-MDO-3
Deshmukh, R., 87-DSC-6
Desmet, W., 9-NDA-1
Dettmer, W., 76-SDM-39
Dhama, R., 50-SDM-22, 51-SDM-23
Di Maio, D., 7-GSF-1
Di Matteo, N., 125-SDM-61
Dias, J., 18-SDM-9, 102-ASC-7
Dillman, R., 121-GSF-8
Dimitriadis, G., 111-SDM-56
Dixit, A., 57-SDM-29
Doepke, E., 137-GSF-9
Domber, J., 7-GSF-1, 109-SDM-54
Domyancic, L., 60-SDM-32, 125-SDM-61
52
Donnelly, P., 70-SDM-33
Dorduncu, M., 31-SDM-13
Dowell, E., 55-SDM-27, 111-SDM-56, 120-DSC-8, 141-SDM-68/GSF-10
Doyle, D., 74-SDM-37, 135-ASC-9
Drake, D., 38-SDM-20
Drazumeric, R., 33-SDM-15
Drela, M., 15-SDM-6
Drummond, F., 45-ASC-3
Duan, B., 8-MDO-1
Duan, Y., 129-SDM-65
DuBien, J., 38-SDM-20
Eacker, C., 105-MDO-7
Eason, T., 87-DSC-6
Eastwood, J., 48-MDO-4
Eden, T., 19-SDM-10
Eger, C., 33-SDM-15, 96-SDM-50
Ehrhardt, D., 94-SDM-48
El Yagoubi, J., 17-SDM-8
Endler, S., 26-GSF-2
Engelstad, S., 12-SDM-3, 70-SDM-33, 124-SDM-60
Enright, M., 11-SDM-2, 49-NDA-4, 113-SDM-58
Erazo, K., 129-SDM-65
Ermanni, P., 24-ASC-2, 27-MDO-2
Erturk, A., 102-ASC-7, 134-ASC-8
Esau, Z., 53-SDM-25
Estevez, J., 114-SDM-59
Eun, W., 75-SDM-38
Fahrenthold, E., 13-SDM-4
FaisalHaider, M., 37-SDM-19
Falcao, L., 5-ASC-1
Fang, E., 60-SDM-32
Fang, H., 26-GSF-2, 67-GSF-4, 121-GSF-8
Faria, C., 24-ASC-2
Fazzolari, F., 142-SDM-69
Felix, L., 122-MDO-9
Feng, D., 129-SDM-65
Ferguson, S., 48-MDO-4, 88-MDO-6
Fernandez, J., 104-GSF-6
Fertig, R., 60-SDM-32, 77-SDM-40
Feszty, D., 75-SDM-38
Fischer, C., 69-NDA-5
Fisher, C., 36-SDM-18
Fitzwater, L., 49-NDA-4, 140-NDA-11
Flansburg, B., 70-SDM-33
Florin, P., 78-SDM-41
Fluck, M., 54-SDM-26
Foerster, C., 31-SDM-13
Footdale, J., 7-GSF-1, 47-GSF-3
Fowler, B., 112-SDM-57
Frecker, M., 24-ASC-2
Freymiller, J., 33-SDM-15
Friedmann, P., 14-SDM-5, 46-DSC-3, 58-SDM-30, 93-SDM-47
Friedrich, L., 92-SDM-46
Friswell, M., 5-ASC-1, 24-ASC-2, 76-SDM-39, 134-ASC-8
Fulcher, J., 121-GSF-8
Furuya, H., 47-GSF-3, 104-GSF-6, 121-GSF-8
Góes, L., 16-SDM-7
Gabb, T., 113-SDM-58
Gallon, J., 36-SDM-18
Gandhi, F., 86-ASC-6, 102-ASC-7
Gangadharan, S., 126-SDM-62
Gardi, R., 112-SDM-57
Gariffo, J., 6-DSC-1
Garnand-Royo, J., 96-SDM-50
Garnich, M., 60-SDM-32
Garza, J., 37-SDM-19
Gauthier Perron, S., 15-SDM-6
Gavin, J., 78-SDM-41
Gdoutos, E., 97-SDM-51
Gemmer, T., 48-MDO-4
Gern, F., 71-SDM-34
Geubelle, P., 66-DSC-4, 97-SDM-51
Ghazizadeh, M., 114-SDM-59
Ghisu, T., 48-MDO-4
Ghoman, S., 76-SDM-39
Ghosh, S., 19-SDM-10
Ghoshal, A., 65-ASC-5
Gibbs, S., 141-SDM-68/GSF-10
Gibbs IV, S., 55-SDM-27
Giurgiutiu, V., 65-ASC-5, 130-SDM-66
Glaessgen, E., 37-SDM-19, 60-SDM-32, 114-SDM-59
Goebel, K., 29-NDA-2, 59-SDM-31
Gogulapati, A., 58-SDM-30
Goldberg, R., 52-SDM-24
Goldsmith, M., 52-SDM-24
Gomes, A., 5-ASC-1, 122-MDO-9
Gong, P., 125-SDM-61
Gong, X., 135-ASC-9
Gonnet, P., 69-NDA-5
Goodmiller, G., 70-SDM-33
Gordnier, R., 58-SDM-30
Gould, K., 80-SDM-43
Goyal, V., 31-SDM-13
Grandhi, R., 8-MDO-1, 69-NDA-5, 106-NDA-7
Grappasonni, C., 72-SDM-35, 129-SDM-65
Grauer, J., 24-ASC-2
Greschik, G., 104-GSF-6, 121-GSF-8
Gresil, M., 130-SDM-66
Griffin, K., 87-DSC-6, 94-SDM-48, 120-DSC-8
Griffith, D., 32-SDM-14, 72-SDM-35, 136-DSC-9
Grigoriev, M., 67-GSF-4
Grosbein, H., 71-SDM-34
Gu, Y., 46-DSC-3
Guan, X., 9-NDA-1, 17-SDM-8, 65-ASC-5
Guerrant, D., 141-SDM-68/GSF-10
Guerreiro, N., 24-ASC-2
Guo, S., 125-SDM-61, 138-MDO-10
Guo, Y., 90-SDM-44
Gurdal, Z., 90-SDM-44, 108-SDM-53
Gurtowski, N., 66-DSC-4
Gururaja, S., 91-SDM-45
Guruswamy, G., 126-SDM-62
Gutierrez, A., 67-GSF-4
Guyer, R., 122-MDO-9
Ha, C., 71-SDM-34
Haase, T., 86-ASC-6
Haftka, R., 8-MDO-1, 28-MDO-3, 52-SDM-24,
107-NDA-8
Hajj, M., 33-SDM-15, 35-SDM-17, 58-SDM-30,
68-MDO-5, 72-SDM-35, 74-SDM-37, 142-SDM-69
Halbert, K., 49-NDA-4, 140-NDA-11
Haldar, S., 31-SDM-13
Hall, C., 36-SDM-18
Hall, K., 58-SDM-30, 74-SDM-37, 120-DSC-8
Hancock, B., 88-MDO-6
Handlin, D., 114-SDM-59
Hanson, C., 111-SDM-56
Hardaway, L., 71-SDM-34
Hartl, D., 135-ASC-9
Hasan, Z., 30-SDM-12, 53-SDM-25
Hasseldine, B., 31-SDM-13
Haupt, M., 16-SDM-7
Havens, D., 105-MDO-7
Hayes, N., 78-SDM-41
He, J., 17-SDM-8, 59-SDM-31
He, L., 49-NDA-4, 59-SDM-31
He, S., 46-DSC-3
Heald, J., 109-SDM-54, 137-GSF-9
Hebert, C., 142-SDM-69
Hedgecock, C., 73-SDM-36
Heeg, J., 103-DSC-7
Heller, R., 76-SDM-39
Henrich, C., 51-SDM-23
Herber, D., 8-MDO-1
Herd, R., 111-SDM-56
Hernandez, E., 129-SDM-65
Hesse, H., 128-SDM-64
Hewson, R., 68-MDO-5
Hill, C., 52-SDM-24
Hillebrandt, M., 104-GSF-6
Hilton, H., 53-SDM-25, 71-SDM-34, 108-SDM-53
Hinkle, J., 47-GSF-3
Hobeck, J., 34-SDM-16
Hoburg, W., 28-MDO-3
Hodges, D., 35-SDM-17, 50-SDM-22, 57-SDM-29, 111-SDM-56
Hodges, T., 26-GSF-2
Hoitink, A., 55-SDM-27
Holland, F., 113-SDM-58
Hollkamp, J., 25-DSC-2
Honea, G., 76-SDM-39
Hoogreef, M., 76-SDM-39
Horst, P., 16-SDM-7
Horvath, Z., 38-SDM-20
Hosur, M., 38-SDM-20
Hrinda, G., 92-SDM-46
Hrishikeshavan, V., 96-SDM-50
Hu, H., 95-SDM-49
Huang, H., 49-NDA-4, 59-SDM-31, 114-SDM-59
Hubbard, J., 24-ASC-2
Huff, G., 45-ASC-3
Hühne, C., 104-GSF-6
Hunt, R.,142-SDM-69
Hurtado, J., 32-SDM-14
Hwang, J., 48-MDO-4
Ifju, P., 135-ASC-9
Ihn, J., 140-NDA-11
Inman, D., 24-ASC-2, 57-SDM-29, 127-SDM-63
Inselberg, A., 88-MDO-6
Islam, M., 10-SDM-1
Jacinto, M., 131-SDM-67
Jacoby, M., 12-SDM-3
Jahan, N., 38-SDM-20
James, S., 31-SDM-13
Jarrett, J., 28-MDO-3, 48-MDO-4
Jeelani, S., 38-SDM-20
Jegley, D., 80-SDM-43
Jenkins, C., 7-GSF-1, 137-GSF-9
Jennings, A., 67-GSF-4, 74-SDM-37, 126-SDM-62
Jensen, G., 18-SDM-9
Jeon, S., 26-GSF-2
Jha, R., 9-NDA-1, 65-ASC-5
Ji, W., 77-SDM-40
Jiang, J., 109-SDM-54
Jiang, P., 138-MDO-10
Jirasek, A., 103-DSC-7
Johanns, W., 32-SDM-14
Johnson, K., 121-GSF-8
Johnson, T., 109-SDM-54, 112-SDM-57
Johnson, V., 130-SDM-66
Jones, D., 142-SDM-69
Jones, S., 130-SDM-66
Joo, J., 24-ASC-2
Jrad, M., 95-SDM-49
Juang, J., 86-ASC-6
Jurewicz, D., 121-GSF-8
Kadonishi, S., 104-GSF-6
Kaiser, B., 13-SDM-4
Kamal, A., 130-SDM-66
Kancharala, A., 134-ASC-8
Kanda, A., 141-SDM-68/GSF-10
Kang, H., 75-SDM-38
Kapania, R., 6-DSC-1, 8-MDO-1, 10-SDM-1, 50-SDM-22, 51-SDM-23, 57-SDM-29, 71-SDM-34, 90-SDM-44, 95-SDM-49, 105-MDO-7, 138-MDO-10
Kapoor, H., 142-SDM-69
Karpel, M., 73-SDM-36, 136-DSC-9
Katsumata, N., 47-GSF-3
Kauffman, J., 127-SDM-63
Kawai, S., 9-NDA-1
Kayran, A., 11-SDM-2
Ke, L., 95-SDM-49
Keating, B., 31-SDM-13
Kelkar, A., 19-SDM-10, 59-SDM-31, 97-SDM-51, 114-SDM-59
Kennedy, G., 27-MDO-2
Kerschen, G., 126-SDM-62
Kessler, S., 78-SDM-41
Khalil, M., 9-NDA-1, 139-NDA-10
Khire, R., 48-MDO-4
Khodaparast, H., 56-SDM-28
Kier, Z., 31-SDM-13
Kim, H., 57-SDM-29, 92-SDM-46, 122-MDO-9
Kim, J., 34-SDM-16
Kim, N., 8-MDO-1, 107-NDA-8, 140-NDA-11
Kim, S., 71-SDM-34
Kim, V., 71-SDM-34, 76-SDM-39
Kim, Y., 137-GSF-9
Kinney, T., 56-SDM-28
Kipouros, T., 88-MDO-6
Kling, A., 108-SDM-53
Kling, D., 47-GSF-3
Kloos, J., 13-SDM-4
Knipe, K., 97-SDM-51
Ko, A., 48-MDO-4
Kobayashi, M., 30-SDM-12
Koch, R., 108-SDM-53
Kogiso, N., 137-GSF-9
Kohlman, L., 52-SDM-24
Kolb, E., 68-MDO-5
Kommers, J., 7-GSF-1
Koo, J., 38-SDM-20, 78-SDM-41
Kosel, T., 33-SDM-15
Kosmatka, J., 34-SDM-16
Krause, D., 55-SDM-27
Krishnamurthy, T., 108-SDM-53, 140-NDA-11
Krueger, R., 11-SDM-2
Kudva, J., 86-ASC-6, 102-ASC-7
53
Kuether, R., 25-DSC-2
Kulak, R., 36-SDM-18
Kulkarni, M., 58-SDM-30
Kumar, D., 93-SDM-47
Kumari, S., 49-NDA-4
Kunz, D., 111-SDM-56
Kusnick, J., 72-SDM-35
Kwak, J., 50-SDM-22
Lachmann, N., 78-SDM-41
LaCroix, B., 135-ASC-9
Lacy, T., 31-SDM-13, 38-SDM-20, 77-SDM-40
Lagoudas, D., 97-SDM-51, 135-ASC-9
Lai, K., 120-DSC-8
Lai, L., 112-SDM-57
Lakshmanan, M., 36-SDM-18
Lal, A., 51-SDM-23
Lambert, L., 136-DSC-9
Lamorte, N., 46-DSC-3
Lan, L., 137-GSF-9
Landman, D., 24-ASC-2
Lao, S., 38-SDM-20
Lappas, V., 104-GSF-6, 121-GSF-8
Lau, F., 5-ASC-1
LaVerde, B.,142-SDM-69
Lawry, M., 33-SDM-15
Lawton, S., 54-SDM-26
Layton, D., 73-SDM-36
Le, C., 94-SDM-48
Le Riche, R., 28-MDO-3, 88-MDO-6
Lee, C., 110-SDM-55, 111-SDM-56
Lee, D., 48-MDO-4
Lee, H., 19-SDM-10, 78-SDM-41
Lee, J., 30-SDM-12, 38-SDM-20, 75-SDM-38
Lee, K., 53-SDM-25
Lee, S., 31-SDM-13
Lenahen, B., 126-SDM-62
Leng, J., 97-SDM-51, 135-ASC-9
LePage, B., 110-SDM-55
Leser, W., 60-SDM-32
Lesieutre, G., 45-ASC-3, 110-SDM-55, 127-SDM-63
Lester, B., 97-SDM-51
Lew, J., 53-SDM-25, 86-ASC-6
Lewis, T., 120-DSC-8
Li, C., 123-NDA-9
Li, D., 138-MDO-10
Li, R., 78-SDM-41
Li, T., 36-SDM-18, 59-SDM-31, 109-SDM-54
Li, Y., 18-SDM-9
Liang, C., 106-NDA-7
Liang, K., 108-SDM-53
Lichodziejewski, D., 121-GSF-8, 141-SDM-68/GSF-10
Liguore, S., 66-DSC-4
Lin, W., 95-SDM-49
Lin, Z., 109-SDM-54
Lind, R., 14-SDM-5, 73-SDM-36
Lindsley, N., 96-SDM-50, 111-SDM-56
Ling, D., 49-NDA-4
Ling, Y., 123-NDA-9
Linton, K., 80-SDM-43
Liu, L., 97-SDM-51
Liu, Q., 138-MDO-10
Liu, T., 114-SDM-59
Liu, Y., 17-SDM-8, 30-SDM-12, 35-SDM-17, 59-SDM-31, 97-SDM-51, 125-SDM-61, 135-ASC-9, 137-GSF-9
Liu, Z., 71-SDM-34, 76-SDM-39
Locatelli, D., 138-MDO-10
Loh, C., 53-SDM-25
Lohner, R., 136-DSC-9
Long, S., 45-ASC-3
Lord, C., 142-SDM-69
Lovejoy, A., 80-SDM-43
Lovelady, K., 37-SDM-19
Lu, J., 18-SDM-9
Lu, Z., 59-SDM-31
Lua, J., 60-SDM-32
Lubineau, G., 17-SDM-8, 52-SDM-24
Luo, S., 114-SDM-59
Lurati, L., 68-MDO-5, 106-NDA-7
Lysher, J., 74-SDM-37
Ma, X., 109-SDM-54
Machairas, T., 135-ASC-9
Madenci, E., 11-SDM-2, 30-SDM-12, 31-SDM-13,
90-SDM-44
Maderuelo, C., 73-SDM-36
Mahadev, S., 30-SDM-12
Mahadevan, S., 69-NDA-5, 106-NDA-7, 123-NDA-9, 140-NDA-11
Maiaru, M., 30-SDM-12
Majumdar, P., 37-SDM-19
Malhan, R., 58-SDM-30
Malla, R., 110-SDM-55, 126-SDM-62
Malladi, V., 135-ASC-9
Mallik, W., 6-DSC-1
Mallol, P., 67-GSF-4
Malusare, K., 77-SDM-40
Mandell, J., 54-SDM-26
Manero, A., 97-SDM-51
Mann, T., 50-SDM-22
Mardanpour, P., 35-SDM-17, 111-SDM-56
Marks, C., 24-ASC-2
Marques dos Santos, F., 16-SDM-7
Marta, A., 27-MDO-2, 48-MDO-4, 55-SDM-27
Martin, B., 127-SDM-63
Martin, R., 92-SDM-46, 109-SDM-54, 112-SDM-57
Martins, J., 27-MDO-2, 48-MDO-4, 58-SDM-30,
105-MDO-7
Marzocca, P., 33-SDM-15, 68-MDO-5, 72-SDM-35
Masarati, P., 58-SDM-30
Mason, J., 74-SDM-37
Materkowski, D., 110-SDM-55
Matlik, J., 113-SDM-58
Matsumoto, J., 104-GSF-6
Matsumura, T., 107-NDA-8
Matsuzaki, Y., 15-SDM-6, 56-SDM-28, 111-SDM-56
Mattson, C., 68-MDO-5, 88-MDO-6
Mavris, D., 71-SDM-34, 76-SDM-39, 86-ASC-6
Maxhimer, K., 112-SDM-57
Mayo, D., 74-SDM-37
Mazzoleni, A., 48-MDO-4
McClung, R., 113-SDM-58
McCullough, K., 53-SDM-25
McEachen, M., 67-GSF-4
McFarland, J., 113-SDM-58
McGowan, D., 5-ASC-1
McLendon, W., 91-SDM-45
McNamara, J., 35-SDM-17, 66-DSC-4, 72-SDM-35, 87-DSC-6
McWilliam, M., 54-SDM-26
Medina, J., 106-NDA-7
Mehmani, A., 88-MDO-6
Mehmood, A., 142-SDM-69
Mejia-Ariza, J., 109-SDM-54
Messac, A., 88-MDO-6
Metlen, T., 125-SDM-61
Meunier, M., 88-MDO-6
Michaeli, M., 71-SDM-34
Mignolet, M., 25-DSC-2
Miller, B., 66-DSC-4
Miller, D., 54-SDM-26
Millwater, H., 37-SDM-19, 49-NDA-4, 107-NDA-8
Min, J., 51-SDM-23, 124-SDM-60
Miskovish, S., 87-DSC-6
Misol, M., 86-ASC-6
Missoum, S., 138-MDO-10
Miyazaki, Y., 104-GSF-6
Modarres, M., 59-SDM-31
Moehle, E., 16-SDM-7
Moens, D., 9-NDA-1
Molavi Tabrizi, A., 143-SDM-70
Molinari, G., 27-MDO-2
Monner, H., 86-ASC-6
Montel, K., 53-SDM-25
Moon, T., 38-SDM-20
Mori, O., 104-GSF-6
Morton, M., 120-DSC-8
Mosquera, A., 24-ASC-2
Moura, M., 34-SDM-16
Muir, E., 93-SDM-47
Muir, M., 68-MDO-5
Mukherjee, I., 74-SDM-37
Mukhopadhyay, V., 76-SDM-39
Mulani, S., 71-SDM-34, 105-MDO-7, 138-MDO-10
Muldal, C., 68-MDO-5
Mullins, J., 123-NDA-9
Mullins, W., 113-SDM-58
Murari, V., 51-SDM-23
Murphey, T., 7-GSF-1, 26-GSF-2, 67-GSF-4
Mustafa, G., 54-SDM-26
Muturi, N., 110-SDM-55, 111-SDM-56
Myers, O., 65-ASC-5, 102-ASC-7
Myrent, N., 72-SDM-35
Nabipour, O., 35-SDM-17
Nadella, K., 65-ASC-5
Nagel, B., 68-MDO-5, 108-SDM-53
Naghipour, P., 91-SDM-45
Nagy, A., 90-SDM-44
Naik, R., 17-SDM-8, 143-SDM-70
Najafi, A., 51-SDM-23, 97-SDM-51
Najafian, H., 136-DSC-9
Nam, S., 71-SDM-34
Nathal, M., 113-SDM-58
Natori, M., 47-GSF-3, 104-GSF-6
Nayfeh, A., 58-SDM-30, 74-SDM-37, 142-SDM-69
Neal, B., 80-SDM-43
Neild, S., 110-SDM-55
Nelson, J., 54-SDM-26, 70-SDM-33
Newman, J., 60-SDM-32
Nguyen Sy, N., 30-SDM-12
Ni, K., 93-SDM-47
Niezrecki, C., 72-SDM-35
Nikbay, M., 30-SDM-12, 103-DSC-7
Ning, X., 92-SDM-46
Nitzsche, F., 35-SDM-17, 75-SDM-38, 87-DSC-6
Noël, J., 126-SDM-62
Norris, A., 105-MDO-7
Nouranian, S., 38-SDM-20
Nucci, M., 87-DSC-6
Nuhait, A., 33-SDM-15, 142-SDM-69
O’Hara, P., 25-DSC-2
O’Hara, R., 68-MDO-5
Obenchain, M., 34-SDM-16, 65-ASC-5
Obitayo, W., 114-SDM-59
Ocampo, J., 49-NDA-4, 60-SDM-32
Ochinero, T., 70-SDM-33
Odermann, F., 108-SDM-53
Ogi, Y., 137-GSF-9
Oh, I., 86-ASC-6
Okasinski, J., 97-SDM-51
Okuizumi, N., 47-GSF-3, 104-GSF-6
Okuma, M., 104-GSF-6
Olliffe, R., 105-MDO-7
Olson, G., 67-GSF-4, 113-SDM-58
Ontiveros, V., 59-SDM-31
Oral, A., 25-DSC-2
Oskay, C., 91-SDM-45
Ostoich, C., 66-DSC-4
Owens, B., 32-SDM-14
Padmanabhan, M., 111-SDM-56
Pai, P., 94-SDM-48, 129-SDM-65
Palacios, J., 19-SDM-10
Palacios, R., 14-SDM-5, 55-SDM-27, 128-SDM-64
Palazotto, A., 19-SDM-10, 68-MDO-5, 125-SDM-61
Pan, E., 143-SDM-70
Panduranga, R., 131-SDM-67
Pankonien, A., 24-ASC-2
Pankow, M., 95-SDM-49
Pant, R., 71-SDM-34
Paquette, J., 32-SDM-14
Park, C., 107-NDA-8
Park, K., 86-ASC-6
Parkes, P., 124-SDM-60
Parkinson, A., 68-MDO-5
Parks, G., 28-MDO-3, 69-NDA-5, 88-MDO-6,
106-NDA-7
Parson, C., 68-MDO-5
Parsons, E., 114-SDM-59
Pasiliao, C., 111-SDM-56
Patel, D., 31-SDM-13
Patil, M., 27-MDO-2, 33-SDM-15, 58-SDM-30,
96-SDM-50
Peeters, B., 16-SDM-7
Pellegrino, S., 26-GSF-2, 47-GSF-3, 67-GSF-4,
92-SDM-46
Pendleton, E., 94-SDM-48
Pendleton, S., 112-SDM-57
Pendse, V., 130-SDM-66
Peng, T., 59-SDM-31
Penmetsa, R., 107-NDA-8
Pepin, J., 123-NDA-9, 139-NDA-10
Perez, R., 25-DSC-2
Peterson, L., 26-GSF-2
Peterson, M., 7-GSF-1, 67-GSF-4
Petrolo, M., 30-SDM-12
Petrovic, M., 137-GSF-9
Phan, N., 90-SDM-44
Philen, M., 134-ASC-8
Piatak, D., 103-DSC-7
Picard, G., 28-MDO-3
Pigazzini, M., 90-SDM-44
Pilato, L., 38-SDM-20
54
Pineda, E., 10-SDM-1, 51-SDM-23, 77-SDM-40, 91-SDM-45
Pingle, P., 72-SDM-35
Pini, M., 106-NDA-7
Pino, J., 32-SDM-14
Pitt, D., 15-SDM-6, 66-DSC-4, 111-SDM-56
Pittman, C., 38-SDM-20
Plaumann, B., 55-SDM-27
Poirel, D., 139-NDA-10
Pollayi, H., 51-SDM-23
Pontecorvo, M., 86-ASC-6, 102-ASC-7
Poplawski, S., 80-SDM-43
Poroseva, S., 13-SDM-4, 29-NDA-2
Postelnicu, E., 124-SDM-60
Potter, C., 71-SDM-34, 76-SDM-39
Powell, D., 95-SDM-49, 131-SDM-67
Prabhakar, P., 77-SDM-40
Pressel, P., 36-SDM-18
Previtali, F., 24-ASC-2
Prosser, D., 136-DSC-9
Przekop, A., 80-SDM-43
Qin, W., 16-SDM-7
Querin, O., 68-MDO-5
Quintana, C., 107-NDA-8
Raghavan, S., 97-SDM-51
Rahman, A., 31-SDM-13
Rais-Rohani, M., 89-NDA-6, 105-MDO-7
Rajagopal, A., 50-SDM-22
Raji, B., 91-SDM-45, 124-SDM-60, 131-SDM-67
Raju, G., 12-SDM-3, 108-SDM-53
Raju, I., 11-SDM-2, 90-SDM-44
Ranatunga, V., 124-SDM-60
Rangaswamy, S., 97-SDM-51
Rankin, C., 12-SDM-3
Ransom, J., 37-SDM-19, 77-SDM-40
Rasmussen, O., 55-SDM-27
Rassaian, M., 52-SDM-24
Raveh, D., 15-SDM-6, 56-SDM-28, 128-SDM-64
Razi, M., 29-NDA-2
Reich, G., 24-ASC-2, 73-SDM-36, 96-SDM-50
Reifsnider, K., 37-SDM-19
Reimerdes, H., 36-SDM-18, 92-SDM-46
Remedia, M., 110-SDM-55
Ren, X., 16-SDM-7
Resor, B., 32-SDM-14
Reyes, M., 136-DSC-9
Rhymer, D., 53-SDM-25
Riazi, M., 75-SDM-38
Ribeiro, P., 34-SDM-16
Ricci, S., 15-SDM-6, 73-SDM-36
Ricciardi, A., 33-SDM-15, 96-SDM-50
Riccobene, L., 15-SDM-6
Richards, J., 96-SDM-50
Richards, P., 35-SDM-17, 111-SDM-56
Richardson, G., 110-SDM-55
Richey, M., 18-SDM-9
Ricks, T., 77-SDM-40
Riddle, T., 54-SDM-26, 70-SDM-33
Righi, F., 135-ASC-9
Riley, M., 105-MDO-7, 139-NDA-10
Riley, Z., 87-DSC-6
Ristow, J., 142-SDM-69
Robbers, B., 112-SDM-57
Roberts, R., 24-ASC-2
Robertson, D., 73-SDM-36, 96-SDM-50
Robertson, G., 68-MDO-5
Robinson, K., 60-SDM-32
Rochow, D., 26-GSF-2
Rogers, J., 46-DSC-3, 135-ASC-9
Rohl, P., 138-MDO-10
Rome, J., 31-SDM-13
Romero, V., 123-NDA-9
Rongong, J., 142-SDM-69
Ross, M., 33-SDM-15
Rothkegel, J., 111-SDM-56
Rouhi, M., 105-MDO-7
Rouse, J., 33-SDM-15
Roy, A., 114-SDM-59
Roy, S., 38-SDM-20, 78-SDM-41, 113-SDM-58
Roybal, M., 30-SDM-12
Rudd, J., 65-ASC-5
Rumpfkeil, M., 69-NDA-5, 88-MDO-6, 89-NDA-6
Russell, S., 52-SDM-24, 71-SDM-34, 76-SDM-39
Ruzzene, M., 129-SDM-65
Ryan, M., 96-SDM-50
Ryu, H., 75-SDM-38
Saam, L., 96-SDM-50
Saavedra Flores, E., 5-ASC-1
Sadat, S., 91-SDM-45, 124-SDM-60, 131-SDM-67
Saghir, S., 17-SDM-8
Sakamoto, H., 104-GSF-6
Salcedo, E., 94-SDM-48
Salehian, A., 127-SDM-63
Samaratunga, D., 65-ASC-5
Samborsky, D., 54-SDM-26
Samur, A., 134-ASC-8
Sandhu, R., 139-NDA-10
Sankar, B., 52-SDM-24
Sankararaman, S., 29-NDA-2, 123-NDA-9
Santer, M., 26-GSF-2, 67-GSF-4
Santhanakrishnan, R., 38-SDM-20
Sanyal, S., 71-SDM-34
Saravanos, D., 135-ASC-9
Sarhaddi, D., 76-SDM-39
Sarkar, A., 9-NDA-1, 139-NDA-10
Satou, Y., 47-GSF-3, 104-GSF-6
Savill, A., 88-MDO-6
Sawada, H., 104-GSF-6
Saxena, A., 59-SDM-31
Sayar, B., 11-SDM-2
Schaub, H., 121-GSF-8
Schenk, M., 104-GSF-6
Scherrer, I., 121-GSF-8
Schervan, T., 36-SDM-18
Schetz, J., 6-DSC-1
Schrage, D., 18-SDM-9
Schreider, L., 26-GSF-2
Schultz, K., 141-SDM-68/GSF-10
Schultz, M., 92-SDM-46
Scigliano, R., 112-SDM-57
Scott, R., 46-DSC-3
Scotti, A., 6-DSC-1
Sebastiano, F., 73-SDM-36
Seeley, C., 72-SDM-35, 134-ASC-8
Seidel, G., 38-SDM-20, 60-SDM-32, 77-SDM-40, 78-SDM-41, 130-SDM-66
Selvakumaran, L., 17-SDM-8
Senba, A., 137-GSF-9
Senda, K., 137-GSF-9
Sengezer, E., 38-SDM-20
Sens, B., 31-SDM-13
Sensmeier, M., 91-SDM-45
Seshadri, P., 69-NDA-5, 106-NDA-7
Shah, P., 87-DSC-6
Shahpar, S., 106-NDA-7
Shankar, R., 113-SDM-58
Sharp, A., 74-SDM-37
Sharpe, M., 131-SDM-67
Shaw, A., 110-SDM-55
Shaw, P., 80-SDM-43
Shen, Y., 130-SDM-66
Shepard, J., 112-SDM-57
Shi, H., 26-GSF-2
Shimada, M., 55-SDM-27
Shimoyama, K., 9-NDA-1
Shin, H., 131-SDM-67
Shin, S., 50-SDM-22, 75-SDM-38
Shirasawa, Y., 104-GSF-6
Shiryayev, O., 16-SDM-7
Shivakumar, K., 11-SDM-2, 17-SDM-8, 59-SDM-31, 97-SDM-51, 131-SDM-67
Shousetrman, A., 73-SDM-36
Shousterman, A., 136-DSC-9
Shtark, A., 71-SDM-34
Sicard, J., 75-SDM-38
Sihn, S., 114-SDM-59
Siljee, D., 97-SDM-51
Silva, T., 102-ASC-7
Silva Neto, A., 78-SDM-41
Silver, M., 137-GSF-9
Simpson, R., 55-SDM-27
Simsiriwong, J., 38-SDM-20
Singh, A., 31-SDM-13
Singh, G., 27-MDO-2, 89-NDA-6
Sinha, S., 13-SDM-4
Sirohi, J., 75-SDM-38
Sivaneri, N., 34-SDM-16, 70-SDM-33
Slater, J., 16-SDM-7, 25-DSC-2, 66-DSC-4, 93-SDM-47
Sleight, D., 109-SDM-54, 112-SDM-57
Smarslok, B., 69-NDA-5
Smith, A., 142-SDM-69
Smith, H., 49-NDA-4
Smith, M., 136-DSC-9
Smith, R., 59-SDM-31
Smith, S., 121-GSF-8, 137-GSF-9
Snyder, R., 27-MDO-2, 58-SDM-30, 86-ASC-6, 102-ASC-7
Sobotka, J., 25-DSC-2
Socrate, S., 114-SDM-59
Sodja, J., 33-SDM-15
Soghrati, S., 97-SDM-51
Soliman, H., 90-SDM-44
Soltis, J., 19-SDM-10
Son, K., 13-SDM-4
Soto, O., 136-DSC-9
Sottos, N., 97-SDM-51
Spak, K., 127-SDM-63
Spies, A., 110-SDM-55, 111-SDM-56
Spottswood, S., 87-DSC-6
Sprague, M., 57-SDM-29, 72-SDM-35
Srinivasan, G., 65-ASC-5
Srivastava, A., 138-MDO-10
Staggers, D., 18-SDM-9
Stanford, B., 6-DSC-1, 122-MDO-9
Stargel, D., 37-SDM-19, 60-SDM-32
Stasiunas, E., 33-SDM-15
Stavely, R., 45-ASC-3
Steckel, G., 31-SDM-13
Steeves, J., 26-GSF-2
Stein, I., 38-SDM-20
Steiner, S., 38-SDM-20, 78-SDM-41
Sternovsky, Z., 121-GSF-8
Stewart, E., 27-MDO-2
Stiles, L., 121-GSF-8
Stohlman, O., 104-GSF-6
Straubel, M., 104-GSF-6
Strganac, T., 32-SDM-14, 56-SDM-28
Stuebner, M., 60-SDM-32
Su, H., 96-SDM-50
Subber, W., 9-NDA-1
Suh, P., 86-ASC-6
Suleman, A., 5-ASC-1, 18-SDM-9, 24-ASC-2,
96-SDM-50, 122-MDO-9
Sullivan, D., 135-ASC-9
Sullivan, R., 38-SDM-20
Sultan, C., 50-SDM-22, 141-SDM-68/GSF-10
Sun, H., 130-SDM-66
Sun, J., 135-ASC-9
Sundaram, S., 74-SDM-37
Sundararaghavan, V., 19-SDM-10
Sunny, M., 50-SDM-22, 71-SDM-34, 95-SDM-49
Surampudi, S., 66-DSC-4, 128-SDM-64
Suryakumar, V., 32-SDM-14, 56-SDM-28
Swenson, E., 109-SDM-54
Swiler, L., 123-NDA-9
Tackett, M., 88-MDO-6
Taflanidis, A., 106-NDA-7
Tagade, P., 69-NDA-5
Taha, H., 58-SDM-30, 68-MDO-5, 74-SDM-37
Talreja, R., 32-SDM-14
Tamilselvan, P., 140-NDA-11
Tamma, K., 55-SDM-27
Tan, H., 137-GSF-9
Tandy, W., 7-GSF-1
Tarazaga, P., 7-GSF-1, 135-ASC-9
Taylor, P., 103-DSC-7
Taylor, R., 11-SDM-2
Teng, C., 143-SDM-70
TerMaath, S., 12-SDM-3, 70-SDM-33
Tessler, A., 30-SDM-12
Tetreault, S., 105-MDO-7
Thacker, B., 29-NDA-2
Thamann, M., 137-GSF-9
Thomas, G., 78-SDM-41
Thomas, J., 120-DSC-8
Thomas, M., 66-DSC-4
Thomsen, M., 76-SDM-39
Thwing, C., 53-SDM-25
Tibert, G., 67-GSF-4
Tiomkin, S., 15-SDM-6
Tipton, D., 33-SDM-15
Toghiani, H., 38-SDM-20
Tojo, B., 27-MDO-2
Tomar, V., 19-SDM-10, 78-SDM-41
Tooley, M., 72-SDM-35
Torng, T., 49-NDA-4, 69-NDA-5, 140-NDA-11
Toropov, V., 28-MDO-3, 68-MDO-5
Towner, R., 127-SDM-63,142-SDM-69
Trease, B., 36-SDM-18
Tummala, Y., 24-ASC-2
55
Tutt, B., 121-GSF-8
Tzong, G., 66-DSC-4
Upadhyay, C., 50-SDM-22, 51-SDM-23
Urbina, A., 123-NDA-9
Usta, R., 89-NDA-6
Vale, J., 5-ASC-1
Vamosi, S., 75-SDM-38
Van Der Auweraer, H., 16-SDM-7
Vandepitte, D., 9-NDA-1
Vasile, M., 89-NDA-6
Vedula, P., 29-NDA-2
Velicki, A., 80-SDM-43
Venkataraman, S., 31-SDM-13, 123-NDA-9
Verhaeghe, W., 9-NDA-1
Vila, L., 126-SDM-62
Villanueva, D., 28-MDO-3
Vincent, H., 38-SDM-20
Viquerat, A., 104-GSF-6
Virakthi, A., 31-SDM-13
Voloshin, V., 68-MDO-5
Vos, R., 76-SDM-39
Waas, A., 19-SDM-10, 31-SDM-13, 51-SDM-23, 77-SDM-40, 95-SDM-49
Wagg, D., 110-SDM-55
Wagner, D., 37-SDM-19
Wagschal, K., 31-SDM-13
Walch, D., 105-MDO-7
Waldman, R., 134-ASC-8
Walsh, T., 33-SDM-15
Wan, Z., 128-SDM-64
Wang, C., 125-SDM-61, 137-GSF-9
Wang, H., 19-SDM-10, 52-SDM-24
Wang, I., 55-SDM-27
Wang, J., 46-DSC-3
Wang, L., 59-SDM-31, 88-MDO-6, 128-SDM-64
Wang, P., 89-NDA-6, 140-NDA-11
Wang, Q., 57-SDM-29, 72-SDM-35
Wang, R., 65-ASC-5
Wang, X., 25-DSC-2
Wang, Y., 14-SDM-5, 52-SDM-24, 57-SDM-29, 140-NDA-11
Wang, Z., 76-SDM-39, 89-NDA-6, 92-SDM-46,
141-SDM-68/GSF-10
Wanthal, S., 60-SDM-32, 77-SDM-40
Wardle, B., 10-SDM-1, 38-SDM-20, 51-SDM-23, 78-SDM-41, 114-SDM-59
Watanabe, A., 47-GSF-3
Waycaster, G., 8-MDO-1
Weaver, P., 12-SDM-3, 108-SDM-53, 110-SDM-55
Weber, J., 32-SDM-14
Weckner, O., 138-MDO-10
Wei, B., 26-GSF-2
Weigand, J., 70-SDM-33
Welsh, W., 6-DSC-1
Wereley, N., 24-ASC-2
Werter, N., 76-SDM-39
Whitcomb, J., 91-SDM-45
White, E., 5-ASC-1, 86-ASC-6, 102-ASC-7
White, S., 97-SDM-51
Whiting, B., 25-DSC-2
Wickramasinghe, V., 55-SDM-27
Wicks, S., 51-SDM-23
Wieseman, C., 103-DSC-7
Wilckens, D., 108-SDM-53
Wilkie, W., 26-GSF-2, 47-GSF-3, 141-SDM-68/GSF-10
Willcox, K., 53-SDM-25
Willey, C., 47-GSF-3
Williams, M., 114-SDM-59
Williams, R., 36-SDM-18, 112-SDM-57
Williams, T., 92-SDM-46
Willis, B., 57-SDM-29, 71-SDM-34, 93-SDM-47, 111-SDM-56
Wilson, L., 47-GSF-3
Wissa, A., 24-ASC-2
Witte, P., 71-SDM-34, 76-SDM-39
Wolfe, D., 19-SDM-10
Wolff, M., 70-SDM-33
Wong, T., 113-SDM-58
Woo, K., 54-SDM-26, 137-GSF-9
Woods, B., 24-ASC-2, 134-ASC-8
Woolsey, C., 96-SDM-50
Wu, H., 80-SDM-43
Wu, K., 92-SDM-46
Wu, W., 113-SDM-58
Wu, Z., 12-SDM-3, 14-SDM-5, 94-SDM-48, 108-SDM-53
Wynn, A., 14-SDM-5
Xiang, J., 76-SDM-39
Xiao, X., 52-SDM-24
Xie, C., 35-SDM-17, 128-SDM-64
Xu, J., 59-SDM-31
Xue, Y., 59-SDM-31
Yamakawa, H., 47-GSF-3
Yamamoto, N., 97-SDM-51
Yancey, B., 32-SDM-14
Yang, B., 26-GSF-2, 121-GSF-8
Yang, C., 14-SDM-5, 35-SDM-17, 94-SDM-48,
128-SDM-64
Yang, J., 17-SDM-8
Yang, S., 114-SDM-59, 131-SDM-67,
141-SDM-68/GSF-10
Yang, Y., 14-SDM-5, 16-SDM-7, 75-SDM-38
Yang, Z., 46-DSC-3
Ye, Z., 50-SDM-22, 143-SDM-70
Yee, K., 75-SDM-38
Yeilaghi Tamijani, A., 138-MDO-10
Yekani Fard, M., 91-SDM-45, 124-SDM-60,
131-SDM-67
Yen, C., 95-SDM-49
Yi, P., 52-SDM-24
Yingtao, Z., 18-SDM-9
Yipaer, F., 141-SDM-68/GSF-10
Yiu, Y., 127-SDM-63
Yokoyama, J., 121-GSF-8
Yokozeki, T., 141-SDM-68/GSF-10
You, Z., 19-SDM-10
Yu, W., 10-SDM-1, 19-SDM-10, 50-SDM-22,
51-SDM-23, 72-SDM-35, 130-SDM-66, 134-ASC-8, 143-SDM-70
YU, Z., 52-SDM-24
Yuan, F., 53-SDM-25, 60-SDM-32
Zafar, N., 8-MDO-1
Zappino, E., 73-SDM-36
Zehnder, A., 31-SDM-13
Zender, F., 18-SDM-9
Zeng, K., 76-SDM-39
Zhang, B., 18-SDM-9
Zhang, J., 9-NDA-1, 88-MDO-6
Zhang, L., 125-SDM-61, 137-GSF-9, 143-SDM-70
Zhang, R., 94-SDM-48
Zhang, W., 17-SDM-8, 59-SDM-31
Zhang, Z., 136-DSC-9
Zhao, S., 134-ASC-8
Zheng, F., 109-SDM-54
Zhimiao, Y., 35-SDM-17, 72-SDM-35
Zhou, S., 9-NDA-1
Zhou, Z., 141-SDM-68/GSF-10
Zhu, S., 49-NDA-4, 59-SDM-31
Zhuang, L., 32-SDM-14
Zhupanska, O., 52-SDM-24, 124-SDM-60
Zill, T., 68-MDO-5, 108-SDM-53
Zink, P., 94-SDM-48
Zipay, J., 53-SDM-25
Zong, Y., 109-SDM-54
Zuchowski, B., 6-DSC-1
Zuowei, W., 36-SDM-18
NOTES
Win
op
FLOOR PLAN
Wh
ite
Lexington
Stanb
thr
St. James
Hil
Newbury
Stanhope
l
Thoreau
Tremont
Stuart
Boston Park Plaza Hotel & Towers
2nd Floor Mezzanine
Lower Lobby
Imperial Ballroom
Terrace
Plaza Ballroom
Geo
rgia
n
ELEVATORS
Lobby
Atrium
Cla
ren
don
Ber
kel
ey
Arli
ngt
on
Statler
Exeter
Fairfield
Hancock
4th Floor
Brandeis
Stairs to
Mezzanine
Franklin
Copley
Emerson
ELEVATORS
Longfellow Holmes
Shawmut
Wh
ittie
r
thr
Stanbro
Win
op
Wh
ite
St. James
Hil
Lexington
Newbury
l
Thoreau
Tremont
Stuart
Stanhope
Gloucester
Alcott
ay
Cabot
Constitution
Charles
River
Beacon Hill
kB
Cambridge
Bac
Board
Room
13–17 January 2014National Harbor, Maryland
(near Washington, D.C.)
See You Next Year!
Abstract Submission DEADLINE: 5 JUNE 2013
www.aiaa.org/scitech2014 • #aiaaSciTech

2013 Final Program - American Institute of Aeronautics and

Transcription

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