apisat-2014 - 2014 Asia-Pacific International Symposium on
Transcription
apisat-2014 - 2014 Asia-Pacific International Symposium on
APISAT-2014 2014 Asia-Pacific International Symposium on Aerospace Technology program(Draft) 24-26 September Shanghai China Hosted by CSAA Chinese Society of Aeronautics and Astronautics Co-organized by RAeS Australian Division of the Royal Aeronautical Society KSAS Korean Society for Aeronautical and Space Sciences JSASS Japan Society for Aeronautical and Space Sciences APISAT-2014 2014 Asia-Pacific International Symposium on Aerospace Technology program Contents Welcome Message from Presdient of CSAA 2 Welcome Message from International ProgramChairman of APISAT 2014 3 About APISAT 4 Organizing Committee 5 Schedule at a Glance 6 Plenary Lectures 7 Invited Lecture 10 Technical Session Program 11 Parallel Session Schedule 14 Registration35 Social Events 37 General Information 40 about shanghai 45 Reception Banquet and performance Post tour Conference Venu13 Transportation Accommodation14 Currency15 Abstracts 3 APISAT-2014 2014 Asia-Pacific International Symposium on Aerospace Technology program 4 Welcome Message from Presdient of CSAA APISAT-2014 2014 Asia-Pacific International Symposium on Aerospace Technology program Welcome Message from International Program Chairman of APISAT 2014 5 APISAT-2014 2014 Asia-Pacific International Symposium on Aerospace Technology program About APISAT Organization The Asia-Pacific International Symposium on Aerospace Technology (abbreviated title: APISAT) is co-organized by the following four societies (in alphabetical order): • Australian Division of the Royal Aeronautical Society (RAeS Australian Division) • Chinese Society of Aeronautics and Astronautics (CSAA) • Japan Society for Aeronautical and Space Sciences (JSASS) • Korean Society for Aeronautical and Space Sciences (KSAS) Aim and Scope Asia-Pacific International Symposium on Aerospace Technology (APISAT) is the collaborative endeavor among the Chinese, Australian, Korean and Japanese societies for aerospace sciences. It provides the opportunity to Asia-Pacific nations for the researchers of universities and academic institutes, and for the industry engineers to discuss the current and future advanced topics in aeronautical and space engineering. The official language of this symposium is English. Topics 6 Topics include but are not limited to: Aerodynamics and Design • Computational Fluid Dynamics • Wind Tunnel Testing • Flow Visualization • Unsteady Aerodynamics • Acoustics • Aircraft, Helicopter and UAV Design Dynamics/Control/Avionics • Flight Simulation • Navigation • Guidance and Control • ATM/CNS • Sensors and Actuators • Satellite Attitude Control Structures and Materials • Structural Analysis • Structural Testing • Smart Structures • Composite Structures • Structural Dynamics • Aeroelasticity Combustion and Propulsion • Combustion Analysis • Fuel Injection • Turbines • Engines • Cooling Systems • Spacecraft Propulsion APISAT-2014 2014 Asia-Pacific International Symposium on Aerospace Technology Executive Committee program Organization Committee Gaozhuo Liu (President, CSAA) Noel Schmidt (President, RAeS Australian Division) Myung Seong Kim (President, KSAS) Seiya Ueno (President, JSASS) International Program Committee Chairman: Haiyan Hu (CSAA) Co-Chairman: Cees Bil (RAeS Australian Division) In Hee Hwang (KSAS) Takeshi Tsuchiya (JSASS) Member: Song Fu (CSAA) Xiaolin Liu (RAeS Australian Division) Jae-Woo Lee(KSAS) Hitoshi Arizono (JSASS) National Organizing Committee (CSAA) Chairman Haiyan Hu Vice Chairman Song Wu Member: Jun Hua, Jun Zhou, Degang Cui, Zhenghong Gao, Weijia Huang, Jinsong Leng, Pinqi Xia, Juen Zhang, Jinxi Ma, Zhihui Tao, Guoqing Wang, Zhiren Han Secretariat Xue Zhang/Ce Yu National Organizing Committee (RAeS Australian Division) Chairman: Cees Bil Member Xiaolin Liu, Don Love, Hideaki Ogawa, Richard Morgan National Organizing Committee (KSAS) Chairman: In Hee Hwang Vice Chairman: Jae-Woo Lee Member Hong-Gye Sung, Jeong-Yeol Choi Secretariat Cheolkeun Ha National Organizing Committee (JSASS) Chairman: Takeshi Tsuchiya Member: Suguru Hase, Masahiro Kanazaki, Takuji Kishimoto, Zhong Lei, Tomoyuki Okita Secretariat: Hitoshi Arizono 7 APISAT-2014 2014 Asia-Pacific International Symposium on Aerospace Technology program Schedule at a Glance Date: Sep. 23-26,2014 Venue: Pullman Shanghai South Hotel Date Sep. 23 Tuesday Sep. 24 Wednesday Sep. 25 Thursday Sep. 26 Friday Time Function 14:00-21:00 On-site registration 08:30-08:45 08:45-09:45 09:45-10:45 10:45-11:00 11:00-12:00 12:00-13:00 13:30-18:40 Opening ceremony Plenary lecture(China) Plenary lecture(Australia) Coffee break Parallel sessions Buffet Parallel sessions 19:00-20:00 Reception 08:45-09:45 09:45-10:45 10:45-11:45 11:45-12:00 Plenary lecture(Korea) Plenary lecture(Japan) Invited lecture (China) Coffee break 12:00-13:00 Buffet 13:30-18:55 19:00-20:30 Parallel sessions Banquet Technical visit to COMAC Shanghai Aircraft Manufacturing Center (SAMC) Lunch Visit Shanghai Museum Dinner Cruise on the Huangpu River Back to the hotel 9:00-11:30 12:00-13:00 14:00-17:00 17:30-18:30 19:00-21:00 21:00 8 Location Hotel Lobby Ballroom 1+2 (3rd floor) Room 1、2、3、5、6、7、8 (3rd floor) Ballroom 3 Room 1、2、3、5、6、7、8 Ballroom 1+2 Coupon is required. Ballroom 1+2 Ballroom 3 Coupon is required. Room 1、2、3、5、6、7、8 Ballroom 1+2 Meet in front of the venue at 9:00. Depart at 9:10 on time. Coupon is required. APISAT-2014 2014 Asia-Pacific International Symposium on Aerospace Technology program Plenary Lecture:September 24 Wednesday 08:45 - 10:45 Lecture 1 China 08:45 - 09:45 Lecture 2 AUSTRALIA 09:45 - 10:45 Development of High-Performance Structural Composites with Mutltifunctionality for Aerospace Application Xiaosu Yi, Director, Science & Technology Committee, Beijing Institute of Aeronautical Materials (BIAM) of AVIC AVIC Composites Center (ACC) Asia-Pacific Air Transport - The next 20 Years John Vincent, BE Aero (Hons) Adjunct Professor at the University of New South Wales Board Director of the Qantas Foundation Memorial Ltd. Plenary Lecture:September 25 Thursday 08:45 - 10:45 Lecture 3 KOREA 08:45 - 09:45 Lecture 4 JAPAN 09:45 - 10:45 Autonomous MultiUAV System for Cooperative Transportation Min-Jea Tahk, Prof.-Division of Aerospace Engineering Korea Advanced Institute of Science and Technology Long-Term Vision of Future Air Traffic Systems in Japan Yutaka Fukuda, Deputy DirectorAir Traffic Management Department Electronic Navigation Research Institute 9 APISAT-2014 2014 Asia-Pacific International Symposium on Aerospace Technology program CHINA Lecture Title Development of High-Performance Structural Composites with Mutltifunctionality for Aerospace Application Lecturer Prof. Xiaosu Yi Affiliation Director, Science & Technology Committee, Beijing Institute of Aeronautical Materials (BIAM) of AVIC AVIC Composites Center (ACC) Mr. Xiaosu Yi received his master degree and doctor degree respectively in 1982 and 1986 in Materials Process Engineering at University of Paderborn, Germany. He became a full professor in Polymer Materials and Technology at Zhejiang University in 1988 and joined Beijing Institute of Aeronautical Materials (BIAM) since 1998, where he has been the member of the executive board and the director of the Science & Technology Committee. He is the Senior Chief Scientist of Aviation Industry of China (AVIC) in composite materials and technology. Prof. Yi received SAMPE FELLOW AWARD in 2011 and became the Academician of APAM (Asia-Pacific Academy of Materials) in 2013. He is also the Chairman of SAMPE Beijing Chapter, the executive council member of International Conference of Composite Materials (ICCM) and Asia-pacific Conference of Composite Materials (ACCM), Vice Chairman of Materials Engineering Committee of Chinese Society of Aeronautics and Astronautics(CSAA), Senior member of the Chinese Composites Society, etc. Prof. Yi is also the chief editor of the Chinese Composite Journal (Acta Materiae Compositae Sinica). He has published about 400 scientific and technical papers in international and domestic journals. About 60 invention patents were awarded to him. His research interests include structural composites, polymer materials, functional composites, process engineering, materials modeling and GREEN material technology. AUSTRALIA Lecture Title Asia-Pacific Air Transport - the Next 20 Years Lecturer Prof. John Vincent Affiliation Adjunct Professor at the University of New South Wales Board Director of the Qantas Foundation Memorial Ltd. John has extensive airline engineering and maintenance experience over a professional career spanning more than 40 years, including more than 25 years in executive and general management roles in large airline Engineering and Maintenance organisations. He is an Aeronautical Engineer, having worked in airline technical services (structures and systems), aircraft performance, fleet assessment and aircraft acceptance/delivery roles. He has filled senior engineering, maintenance, fleet development, safety, quality and risk management roles including holding various National Airworthiness Authority (CASA) approvals and has led the Engineering and Maintenance businesses of Air Pacific (Fiji), Ansett Australia and Qantas Airways Ltd. His main career focal areas have been leadership development, business strategy, business process improvement, change management, governance, regulatory compliance, operational and occupational safety systems, risk management, employee engagement/communication and relationship management. He is Adjunct Professor with the University of New South Wales School of Aviation, a Board Director of the Qantas Foundation Memorial Ltd and President-elect of the Royal Aeronautical Society Australian Division. He is now an executive consultant providing services to the aviation and broader engineering communities. 10 APISAT-2014 2014 Asia-Pacific International Symposium on Aerospace Technology Lecture Title Autonomous Multi-UAV System for Cooperative Transportation Lecturer Prof. Min-Jea Tahk Affiliation Professor, Division of Aerospace Engineering Korea Advanced Institute of Science and Technology (KAIST) program KOREA Education Prof. Tahk received his doctor and master degree in Aerospace Engineering at The University of Texas in 1986 and 1983. He gained his bachelor degree in Aeronautical Engineering at Seoul National University in 1976. He once worked as research scientist at Integrated Systems, Inc, USA from 1987 to 1989 and research engineer at Agency for Defense Development, Korea from 1976 to 1981. Prof. Tahk joined KAIST Division of Aerospace engineering in 1989 and worked as Assistant Professor from 1989-1991, Associate Professor from 1991-1999 and Professor since then. Prof. Tahk is a Technical Editor at IEEE Tr. Aerospace and Electronic Systems since 2011 and once served as Associate Editor there for five years before that. He has been a member of the Editorial Board, Engineering Optimization, Taylor & Francis since 2004. During 2005 and 2011, he was an Associate Editor for Control Engineering Practice, IFAC, Elsevier His academic and advisory activities include: 2013.10-2015.10, Member, National Space Committee 2013-2014, President, Korea Unmanned Vehicle Systems Association (KUVS) 2012, President, The Korea Society for Aeronautics and Space Sciences (KSAS) 2010-2011, Vice President, The Korea Society for Aeronautics and Space Sciences (KSAS) 2010, Vice President, Institute of Control, Robotics and Systems (ICROS) 2009, International Program Committee Co-Chair, The 60th International Astronautical Congress, Daejeon, 2009 (IAC) 2007-2012, Vice President, Korea Unmanned Vehicle Systems Association (KUVSA) 2007-2008 Vice President, Institute of Control, Automation and Systems Engineers (ICASE) 2007-2008, Director, Society of Instrument and Control Engineers (SICE) 2007, Organizing Committee Chair, International Conference on Control, Automation and Systems (ICCAS 2007) 2004, Program Chairman, 2004 KSAS-JSASS Joint Symposium on Aerospace Engineering JAPAN Lecture Title Long-Term Vision of Future Air Traffic Systems in Japan Lecturer Mr. Yutaka Fukuda Affiliation Deputy Director, Air Traffic Management Department Electronic Navigation Research Institute Yutaka Fukuda is the Deputy Director of the ATM (Air Traffic Management) Department at the ENRI (Electronic Navigation Research Institute). The ENRI is responsible for research and development in the field of ATM in Japan, supporting the JCAB (Japan Civil Aviation Bureau). He serves on CARATS (Collaborative Actions for Renovation of Air Traffic Systems) Research and Development Promoting Subcommittee. He has studied airborne collision avoidance system, arrival management, oceanic flexible route system, conflict management and trajectory management after joining ENRI. He was a visiting researcher at the NASA Ames Research Center in 1995. He received a MS degree in Electronics from Tokyo Institute of Technology in 1986 and a BS degree in Electronics from Tokyo Institute of Technology in 1984. 11 APISAT-2014 2014 Asia-Pacific International Symposium on Aerospace Technology program Invited Lecture:September 25 Thursday 11:00-12:00 CHINA 11:00-12:00 The Concept and Principle of Next Generation Aircraft's Mission System Dr. Guoqing Wang President,AVIC Aeronautical Radio Electronics Research Institute CHINA Lecture The Concept and Principle of Next Generation Aircraft's Mission System Lecturer Dr. Guoqing Wang Affiliation President,AVIC Aeronautical Radio Electronics Research Institute Mr. Wang Guoqing, Ph.D, research fellow. Mr. Wang graduated from Northwestern Polytechnical University, received a doctor's degree in computer science and technology, and as doctoral tutor of Northwest Polytechnology University of China since 2000. He was the president of Aeronautic Computing Technology Research Institute ( ACTRI) of China from 2004 to 2008. He is the president of China National Aeronautical Radio Electronics Research Institute ( CARERI ) since 2008. Mr. Wang’s main professional directions of are integrated avionics system,avionics system architecture, integrated modular avionics ( IMA ) system, distributed parallel signal processors, distributed parallel processing, high reliability fault redundant computer, and computer networks. Mr. Wang’s major published books and papers are: 1."Civil Aircraft Avionics Systems", Shanghai Jiaotong University Press of China, 2011. 2."Date Fusion Research Of integrated Modular Avionics System", Intelligent Data Engineering International Conference of China, 2011. 3."Integration Technology For Avionic System", the 31rd Digital Avionics Systems Conference ( DASC 31), 2012. 4."Research on the Architecture Technology for New Generation Integrated Avionics System", 2013 AIAA Aviation 5."Research on Distribute Integrated Modular Avionics System Architecture Design and Implementation ", the 32rd Digital Avionics Systems Conference ( DASC 32), 2013. 12 APISAT-2014 2014 Asia-Pacific International Symposium on Aerospace Technology program Technical Session Program 13 Opening Ceremony at Ballroom 1+2, Addressed by Haiyan, Hu, VP of CSAA 08:30-08:45 19:00-20:30 18:25- 18:40 18:10-18:25 17: 55-18:10 17:40-17:55 17:30 -17:40 17:25-17:30 17:15-17:25 17:10-17:15 17:00-17:10 15:45-17:00 15:25 -15:45 14:40-15:25 14:30-14:40 13:30 -14:30 12:00 -13:00 11:00 -12:00 10:45-11:00 09:45-10:45 08:45-09:45 1-5 Aircraft System Break 1-4 Aircraft Design and Optimization 2 1-3 Aircraft Design and Optimization 1 1-2 UAV 2 1-1 UAV 1 ROOM1 5-3 Structural Optimization (3) 5-5 Aeronautical Materials Break Reception at Ballroom 1+ 2 Mechanics2 3-5 Flight Break Break 5-4 Fatigue and Fracture Coffee Break 3-3 CFD Algorithms 1 3-4 CFD Algorithms 2 2-5 GNC of UAV:Toward Practical Missions 5- 1 Structural Simulation 5-2 General Design Break 3-2 Aerodynamic Optimization and Design 2 2-4 Design of controller 2-3 Avionics Application 2-2 Advanced Design/Simulation and Methods 3-1 Aerodynamic Optimization and Design1 2-1 Advanced Aerodynamic Measurement and Visualization Technology ROOM 5 Lunch at Ballroom 3 ROOM 3 ROOM 2 Coffee Break 6-5 Combustion 3 Break 6-4 Combustion 2 6-3 Combustion 1 6-2 Aircraft Engine System 2 6-1 Aircraft Engine System 1 ROOM 6 7-5 Acoustics Break 7-4 Experimental Techniques and Applications 3 7-3 Experimental Techniques and Applications 2 7-2 Experimental Techniques and Applications 1 7-1 Aeroelasticity(4) ROOM 7 "Plenary Lecture at Ballroom 1+2 ""Development of High-Performance Structural Composites with Mutltifunctionality for Aerospace Application"", Prof. Xiaosu Yi, Director, AVIC BIAM and AVIC Composites Center (ACC), China" "Plenary Lecture at Ballroom 1+2: ""Asia-Pacific Air Transport - the next 20 Years"", Prof. John Vincent, University of New South Wales Board Director of the Qantas Foundation Memorial Ltd., Australia" On site registration outside Ballroom 1+2 07:30-08:00 8-7 Flight Quality, Fault Diagnosis and Tolerant Control 8-6 Control Theory and Analysis 8-4 Guidance Control 8-5 Guiance Technology 8-3 Air Traffic Management 2 8-2 Air Traffic Management 1 8-1 Flight Mechanics1 ROOM 8 Sep.24 Wed program 14 APISAT-2014 2014 Asia-Pacific International Symposium on Aerospace Technology 18:40-18:55 18:25-18:40 18:12-18:25 18:10-18:15 18:00-18:10 17:55-18:00 17:45-17:55 17:40-17:45 17:30-17:40 17:20-17:30 17:10-17:20 17:00-17:10 16:30-16:45 16:45-16:55 16:55-17:00 16:10-16:30 16:05-16:10 16:00-16:05 15 19:00-20:30 1-10 Cooling System 1-9 Cost engineering Break 1-8 Aircraft Aerodynamics3 Coffee Break 15:40-15:55 15:55-16:00 1-7 Aircraft Aerodynamics2 1-6 Aircraft Aerodynamics 1 ROOM1 ROOM 2 ROOM 3 2-9 Target Identification Technique Break 2-8 GNC of Spacecraft Coffee Break 3-9 Simulation of Aerodynamic Heating Break 3-8 Simulation of Unsteady Aerodynamics Coffee Break 5-10 Composite Materials Break 5-9 Jet Flows 5-8 Structural Dynamics and Aerodynamics 5-7 Aeronautical Structural Manufacture and Test Break 5-6 Flight Mechanics3 ROOM 5 ROOM 6 ROOM 7 7-7 Fluid -Structure Coupling 7-8 Flow Control 1 6-9 Spacecraft Propulsion System 2 7-9 Flow Control 2 Break 6-8 Spacecraft Propulsion System 1 Coffee Break 6-7 Flight Simulation 7-6 Conceptual 6-6 Turbine and Heat Design and Trasnfer Evaluation Methods Banquet at Ballroom 1+ 2 2-7 GNC of Miniature 3-7 CFD Applications Aircraft 2 2-6 New Methods of 3-6 CFD Applications Navigation,Estimate 1 and Tracking Lunch at Ballroom 3 Invited lecture: Lecture title TBD, Dr. Guoqing Wang, China National Aeronautical Radio Electronics Research Institute, China 14:40-15:40 14:30-14:40 13:30-14:30 12:00-13:00 11:00-12:00 Coffee Break 8-11 Intelligent Computing, Communication and Control Break 8-10 Simulation of Hypersonic Cases 8-9 Aerodynamic Studies of Power Systems 2 8-8 Aerodynamic Studies of Power Systems 1- 2 ROOM 8 Plenary Lecture: "Long-Term Vision of Future Air Traffic Systems in Japan", Mr. Yutaka Fukuda, Electronic Navigation Research Institute, Japan 09:45-10:45 Sep.25 Wed program 10:45-11:00 Plenary Lecture : "Autonomous Multi-UAV System for Cooperative Transportation", Prof. Min-Jea Tahk, KAIST, Korea 08:45-09:45 APISAT-2014 2014 Asia-Pacific International Symposium on Aerospace Technology Parallel Session Schedule DAY1 Time Paper NO Title Paper ID Session1-1 UAV 1 11:00-12:00 11:00-11:15 01-01-1 11:15-11:30 01-01-2 11:30-11:45 01-01-3 11:45-12:00 01-01-4 Calculation and Analysis on Stealth and Aerodynamics Characteristics of a Medium Altitude Long Endurance UAV Su Haoqin, Bao Xiaoxiang , Li Jianhua , Liu Kai, Cen Mengxi, Song Jing The 11th Department of China Academy of Aerospace Aerodynamic, China Development and Analysis of Project Based Learning Constructing Indoor Unmanned Aerial Vehicle Juri Kimura, Koji Miki, Yasuko Nakamuta, Shinji Suzuki The University of Tokyo, Japan Trajectory Design for Target Localization by UAVs with Bearing-Only Sensor Jaehwan Pi , Hyochoong Bang Korea Advanced Institute of Science and Technology, Korea Aerodynamic Analysis of Duct Shape for VTOL Ducted Fan UAV Minhyoung Ryu, Leesang Cho, Jinsoo Cho, Hanyang University, Korea (68) (283) (297) (325) Session1-2 UAV 2 13:30-14:30 13:30-13:45 01-02-1 13:45-14:00 01-02-2 14:00-14:15 01-02-3 14:15-14:30 01-02-4 Arrowhead-Research on Design of Compound-UAV with Fenestron Shen Wei, Hou Lili Aircraft Design and Research Institute of AVIC Harbin Aircraft Industry Group Co., LTD. China Improving Electric Powered UAVs'Endurance by Incorporating Battery Dumping Concept Tan Chang, Hu Yu Northwestern Polytechnical University, China Development of Efficient Design Synthesis Method for High Altitude Long Endurance UAV system Jeong A Yang, Kwon-Su Jeon, Jae-Woo Lee and Sangho Kim Konkuk University, Seoul, Korea The Multidisciplinary Design Optimization Process and Design Framework Development for the Unmanned Gliding Vehicle Kwon-su Jeon, Maxim Tyan, Sung Hyun Jin, Seong Jun Cho, and Jae-Woo Lee Konkuk University, Korea (361) (341) (443) (444) Session1-3 Aircraft Design and Optimization 1 14:40-15:25 14:40-14:55 01-03-1 14:55-15:10 01-03-2 15:10-15:25 01-03-3 Design, Modeling and Analysis of a Sharp-Edge Hypersonic Stealthy Re-entry Vehicle Guofu Liu, Daochun Li, Jinwu Xiang, Wenli Luo Beijing University of Areonautics and Astronautics, China Introduction of integrated satellite design and analysis software, KARI Satellite Design Software Min Ki Kim Korea Aerospace Research Institute, Korea Behavior of tether for captive stratosphere platform using airship Kazuhisa Chiba, Shin Satori, Ryuichi Mitsuhashi, Hokkaido University of Science, Japan Jun'ya Sasaki, Ryojiro Akiba, Hokkaido Aerospace Science and Technology Incubation Center, Japan (336) (342) (345) Session1-4 Aircraft Design and Optimization 2 15:45-17:15 15:45-16:00 01-04-1 16:00-16:15 01-04-2 16:15-16:30 01-04-3 16:30-16:45 01-04-4 16:45-17:00 01-04-5 EKF Based Wind Velocity Estimation without an Airspeed Sensor for Unpowered Gliding Vehicle Yong-Gonjong Park, Chan Gook Park Seoul National University, Korea An Integrated Platform for Aircraft Conceptual Design and Optimization Yuandong Zhao, Haixin Chen,, Yufei Zhang Tsinghua University, China Research on Multi-Specialty Coordination, Multi-Discipline and Multifunction Integration Oriented Modeling and Simulation Innovation Fan Lin Cao, Baohong Liu, YifeiYao,, Xionghua AVIC the first aircraft institute, China Design and Simulations of a Guide-Screw Hand-Spike Nose Deflecting Mechanism Handong Hu, Liangxian Gu, Xiaofeng Sun, Yifan Song, Xiangpeng Shi National Key Laboratory of Aerospace Flight Dynamics, Northwestern Polytechnical University, China A Reliability Prediction method based on Simulation Analysis Luo xuegang, China Aero-Polytechnology Establishment, China (353) (188) (54) (208) (459) 17:00-17:15 01-04-6 A Study of Closed Loop Control of Active Technique for Helicopter BVI Noise Reduction KOBIKI Noboru, Shigeru SAITO, JAXA, Japan (473) Session1-5 Aircraft System 3 17:25-18:10 17:25-17:40 01-05-1 17:40-17:55 01-05-2 17:55-18:10 01-05-3 The Application of Tooth Contact Analysis in the Shaper Modification for Face-gear Canhui WU, Ping CAO, China Aero-polytechnology Establishment, China Research on Probabilistic Safety Analysis Approach of Flight Control System based on Bayesian Network Chen Kang, Lu Zhong, Nanjing University of Aeronautics & Astronautics, China Zeng Haijun, Nanjing University of Aeronautics & Astronautics, China Research and Development Center, AVIC COMMERCIAL AIRCRAFT ENGINGE CO., LTD., China The Role of Electromagnetic Compatibility Qualification-Considerations in Airborne System Integration Programs Huiying Li, Mark Bolsover, Junhui Ye, Linfang Yan Shanghai Aircraft Design and Research Institute, China (59) (349) (430) Session2-1 Advanced Aerodynamic Measurement and Visualization Technology 11:00-12:00 11:00-11:15 02-01-1 11:15-11:30 02-01-2 11:30-11:45 02-01-3 11:45-12:00 02-01-4 Dimensional Measurement of Small Hot Pieces Based on a Monochrome CCD Bi Chao, Qu Xinghua, Liu Yong, Liu Yaping, Liu Jingliang Aviation Key Laboratory of Science and Technology on Precision Manufacturing Technology, Beijing Precision Engineering Institute for Aircraft Industry, China State Key Laboratory of Precision Measuring Technology and Instrument, Tianjin University, China Design and Calibration of a Six-axis Force/torque Sensor with Large Measurement Range used for the Space Manipulator Danfeng Chen, Aiguo Song, Ang Li, Southeast University, China Research on 3D Virtual Environment Modeling Technology for Space Telerobot Biyu Zhu, Aiguo Song, Xiaonong Xu, Song Li, Southeast University, China Sapphire Fiber-Optic Temperature Sensor Based on Black-Body Radiation Law Wangwei, Shi Xiaotian, Wang Ying China Academy of Aerospace Aerodynamics, China (37) (96) (100) (122) Session2-2 Advanced Design/simulation and Methods 13:30-14:30 13:30-13:45 02-02-1 13:45-14:00 02-02-2 14:00-14:15 02-02-3 14:15-14:30 02-02-4 The test verification design method based on rapid prototyping technology for aero-engine Xiao-Jie Qiu, Wen-Hua Zheng, Yu-Ting Tang, Feng Lu AVIC aviation motor control system institute, China The Nanjing University of Aeronautics & Astronautics, Nanjing, 210016,china Predictive Sliding Mode Control using Feedback Linearization for Hypersonic Vehicle Xianlei Cheng, Peng Wang, Luhua Liu, Guojian Tang, National University of Defense Technology, China Prediction of Large Deformation on Wing Based on Strain Sensors for Array Antenna Signal Compensation Sunghyun Park, Hansol Lee, Yoon-Seon Choi In-Gul Kim, Jong-Myong Woo Chungnam National University, Korea Oo-Chul Jun, Agency for Defense Development, Korea Monte Carlo Analysis for Significant Parameters Ranking in RLV Flight Evaluation Jie GU, Shuguang ZHANG , Baoyin WANG Beihang University, China (63) (285) (306) (382) Session2-3 Avionics Application 14:40-15:25 14:40-14:55 02-03-1 14:55-15:10 02-03-2 Application of Optimal Smoothing to Beamforming Tracking Data based on a Singer Model Junho Jeong, Gyeonghun Kim, Seungkeun Kim, Unmanned Systems Group, Chungnam National University, Korea Jong-Soo Choi ,Yeong-Ju Go, Jaehyung Lee, Aerodynamics and Aeroacoustics Laboratory, Chungnam National University, Korea Wireless optical communication in formation flight of CubeSat using convergent beam Hyun Cheol Jeon, Seoul National Universit, Korea Chan Gook Parkb ,bDepartment of Mechanical and Aerospace Engineering/ Automation and Systems Research Institute, Korea (495) (205) 15:10-15:25 02-03-3 Experimental application of Impoved Hilbert Huang Transform for the detection of air-gap eccentricity in induction motors Jihyoung Cha, Sangho Ko Korea Aerospace University, Korea (376) Session2-4 Design of controller 15:45-17:00 15:45-16:00 02-04-1 16:00-16:15 02-04-2 16:15-16:30 02-04-3 16:30-16:45 02-04-4 16:45-17:00 02-04-5 Research on the New Airplane Develop System Based on 3D-Digital Technique and Multi-Companies Collaboration Wang QianpingFan Lin WuXuhui, AVIC the first aircraft institute, China Anti measure noise research of Morphing wing UAV Su Haoqin, Bao Xiaoxiang, , Shi Hongwei, Liu Kai, Song Jing The 11th Department of China Academy of Aerospace Aerodynamic, China Flight Control Design Using H∞ Control Method for a Single-Propeller UAV Satoshi Kono, Kenji Uchiyama, Nihon University,, Japan Model Predictive Flight Controller Using Prior Air Disturbance Information Obtained By Doppler LIDAR Seiya Miyagaki , Shinji Suzuki,University of Tokyo, Japan Neural Network Controller Design for a Single Tilt-wing UAV Seonghun Yoon, Seungkeun Kim and Jinyoung Suk, Chungnam National University, Korea (67) (51) (212) (232) (273) Session2-5 GNC of UAV:Toward Practical Missions 17:10-17:55 17:10-17:25 02-05-1 17:25-17:40 02-05-2 17:40-17:55 02-05-3 Implication of Dynamic Unbalance to the Inertial Accelerometer Calibration with Vibrafuge Xue-Ming Dong, Changcheng Institute of Metrology and Measurement (CIMM), China Wei Guan, Xiao-Feng Meng, Science and Technology on Inertial Laboratory of Beihang University (BUAA), China A Moving Target Indication Algorithm Adaptable to Illuminance Variation Using the Histogram Matching Seung-Gyu Yun, Sangchul Lee, Sangho Ko School of Aerospace and Mechamical Engineering, Korea Aerospace University, Korea Solutions to Improve Multiple Configuration Systems Resolution in Sensors LIU Hua , DING Quanxin, Luoyang Institute of Electro-optical Equipment of AVIC, China ZHOU Liwei, Beijing Institute of Technology, China (133) (328) (393) Session3-1 Aerodynamic Optimization and Design 1 11:00-12:00 11:00-11:15 03-01-1 11:15-11:30 03-01-2 11:30-11:45 03-01-3 11:45-12:00 03-01-4 Supercritical Natural Laminar Flow Airfoil Optimization Xiaoming Fang, Yufei Zhang and Haixin Chen , Tsinghua University, China Optimal Design of High Power Centrifugal Compressor Using Multi-Objective Genetic Algorithm Hyun-Su Kang, Youn-Jea Kim, Sungkyunkwan Univerisity, Korea. Numerical Study on Vortex Alleviation of Chipped Wings Nahyeon Roh, Sejong Oh, Pusan National University, Busan, Korea Kwanjung Yee, Seoul National University, Seoul, Korea Effects of Trailing Edge Thickness on the Aerodynamic Characteristics of NACA Symmetric Airfoil Wanghyun Kim, Gimyeong Ryu, Byoungsoo Kim, Chungnam National University, Korea (316) (319) (348) (370) Session3-2 Aerodynamic Optimization and Design 2 13:30-14:30 03-02-1 Optimization of Suction Control on an Airfoil Using Multi-islands Genetic Algorithm D.J. Zhao, Y.K. Wang, W.W. Cao, P. Zhou Beijing University of Aeronautics and Astronautics, China (411) 13:45-14:00 03-02-2 Parameter optimization research on lift-enhancing of multi-element airfoil using air-blowing Yuqin Jiao, Yan Lu National Key Laboratory of Science and Technology on Aerodynamic Design and Research, Northwestern Polytechnical University, China (15) 14:00-14:15 03-02-3 Study on Drag Divergence Characteristics of Supercritical Airfoil Ruihuan LIU, Yufei ZHANG, Haixin CHEN School of Aerospace Engineering, Tsinghua University, Beijing, 100084, China (201) 14:15-14:30 03-02-4 Multi-Objective Aerodynamic Optimization of Supercritical Wing with a Large Number of Constraint ZHAO tong, ZHANG Yufei, CHEN Haixin, Tsinghua University, China (255) 13:30-13:45 Session3-3 CFD Algorithms 1 14:40-15:25 17:00-17:15 03-04-6 Verification of a Chemical Nonequilibrium Flows Solver Using The Method of Manufactured Solutions Li Wang, Wei-jiang Zhou ,Chu-qun Ji China Academy of Aerospace Aerodynamics,,China 17:15-17:30 03-04-7 Numerical Prediction of Stability Derivatives for Complex Configurations Fangjian Wang, Lan Chen China Academy of Aerospace Aerodynamic, China (477) 03-03-3 A Modification technique of Collision Probability in the Direct Simulation Monte Carlo Method Huang Fei, Li Peng-fei,Jin Xu-hong, Liu Xiao-wen,Cheng Xiao-li China Academy of Aerospace Aerodynamics, China (176) 15:45-16:00 03-04-1 Design and dynamic analysis of micro-vibration isolator for Single Gimbal Control Moment Gyro Shenghao Shi; Dongxu Li; Qing Luo College of Aerospace Science and Engineering, National University of Defense Technology, China (191) 16:00-16:15 03-04-2 A 3D Anisotropic Cartesian Grid Generation Method and Its Applications in Viscosity Flows Xiaotian Shi, Shuai Fang, Meng Lv, Ning Hu China Academy of Aerospace Aerodynamics, China (215) 16:15-16:30 03-04-3 Evolutionary maintenance based on maintenance free operating period philosophy Ming Xu, Yueqin Wu, China Aero-Polytechnology Establishment, China (221) 16:30-16:45 03-04-4 Influence of high-temperature air on Three-dimensional Nozzle structure design Bu Junhui, China Academy of Aerospace Aerodynamics, China Liu Huaiyin, China Academy of Aerospace Aerodynamics, China (228) 16:45-17:00 03-04-5 An Immersed Boundary Method Based on the Volume Fraction Yuelong He, Dun Li, Shuai Liu and Handong Ma China Academy of Aerospace Aerodynamics, China (384) 17:10-17:25 03-05-1 Modified discrete vortex method to simulate the unsteady aerodynamics of two-dimensional insect-like flapping wing models in hover Anh Tuan Nguyen, Jae-Hung Han KAIST, Korea (190) 17:25-17:40 03-05-2 Satellite Formation Flying using Low Thrusters and Solar Sail YeerangLim, Hyochoong Bang, KAIST, Korea (195) 17:40-17:55 03-05-3 Prediction of Projectile Trajectories Launched from Helicopter Hyojoon Gong, Seungsoo Lee, Inha University, Korea Jae Seong Park, Agency for Defense Development, Korea (263) 03-05-4 Control surface characteristics of the small-scale supersonic flight experiment vehicle (OWASHI) of Muroran-IT Yoshihiro Suzuki, Sakae Oishi, Kazuhide Mizobata, Nobuhiro Tanatsugu Muroran Institute of Technology, Japan Takakage Arai, Osaka Prefecture University, Japan (269) 15:10-15:25 (417) Session3-4 CFD Algorithms 2 15:45-17:00 Session3-5 Flight Mechanics2 17:10-18:10 17:55-18:10 Session5-1 Structural Simulation 11:00-12:00 11:00-11:15 05-01-1 Design and simulation of long slender end mill embedded with passive damper Yiqing Yang, Yu Yu, Beihang University, China (184) 11:15-11:30 05-01-2 TC4 Hollow Fan Blade Structural Optimization Based on Bird-Strike Analysis Zeng Chuan, Jiang Xiang-hua, School of Jet Propulsion BUAA, China (223) 11:30-11:45 05-01-3 Six-DOF Modeling and Simulation for Generic Hypersonic Vehicle in Reentry phase Chao Wang ,Xinyu Liu, Feng Li China Academy of Aerospace Aerodynamics(CAAA), China (234) 05-01-4 Test Particle Monte Carlo Simulation of Return Flux on Various geometric surfaces due to Ambient Scatter of Outgassing Molecules Xuhong Jin, Fei Huang, Zhi Chen, Xiaoli Cheng China Academy of Aerospace Aerodynamics, China (335) 11:45-12:00 Session5-2 General Design 13:30-14:30 05-02-1 Optimal WVR Air-to-Air Combat Maneuver Generation Algorithm using Scoring Function based on Security Strategy Hyunju Park, Dong-Wan Yoo, Min-Jea Tahk Division of Aerospace Engineering, KAIST, Daejeon, Korea (236) 13:45-14:00 05-02-2 Conceptual Design of Single-stage Rocket Using Hybrid Rocket by Means of Genetic Algorithm Masahiro Kanazaki, Tokyo Metropolitan University, Japan Atthaphon Ariyairt, Kazuhisa Chiba, Hokkaido University of Science, Japan Koki Kitagawa, Toru Shimada, Japan Aerospace Exploration Agency, Japan (426) 14:00-14:15 05-02-3 Safety of Lap-Held Infants in Aircraft Cees Bil, Adam Shrimpton, Graham Clark, RMIT University, Australia (460) 14:15-14:30 05-02-4 Design and Optimisation of Electromagnetic Tricycle Operated in Airport (470) 13:30-13:45 Session5-3 Structural Optimization 14:40-15:25 14:40-14:55 05-03-1 Multidisciplinary Design Optimization of Turbine Disks Based On ANSYS Workbench Platforms Qi Xiaodong, AVIC Commercial Aircraft Engine Co. Ltd., Shanghai, China Shen Xiuli, BUAA, China 14:55-15:10 05-03-2 Topology Optimization Method Research on Hollow Wide-Chord Fan Blade of a High-Bypass Turofan Engine J. MENG, L.F. Liao, D. Li, Y. Cao, L.Y. Yang, Y.Y. Chen, ACAE, China (111) 15:10-15:25 05-03-3 Optimal Design Aircraft Engine Mounts Jiang Xianghua,Du Ran, BeiHang University, China (288) (29) Session5-4 Fatigue and Fracture 15:45-17:15 15:45-16:00 05-04-1 16:00-16:15 05-04-2 16:15-16:30 16:30-16:45 16:45-17:00 17:00-17:15 Essential Work of Fracture of Ductile Polymer Membranes Hongsu Bae, Kyeongsik Woo,Chungbuk National University, Korea Hyung-Soon Cho, Jin-Ho Rho, Soo-Yong Lee, Korea Aerospace University, Korea Fatigue Damage Monitoring of an Aluminum Joint Specimen Cui Ronghong, He Yuting, Jing Bo, Hou Bo, Air Force Engineering University, China (276) (106) 05-04-3 Failure Analysis Of Rubbing Of The Fan Tip And Case Of A Engine Feifei Wei, Yunyong Chen, Zhiqing WU, Lulu Chen, Jin Meng R&D Center Dept. of Compression System, AVIC COMMERICAL AIRCRAFT ENGINE CO.,LTD.,China (154) 05-04-4 Statistical Approach to Determine Continuum Damage Weibull Parameters in Laminate Composites Kook Jin Park,Hee-jin Kang,SangJoon Shin, ,Seung Jo Kim, Seoul National University, KOREA Ik-hyun Choi,MinKi Kim, Korea Aerospace Research Institute, KOREA (303) 05-04-5 Prediction of Low Cycle Fatigue Crack Growth under Mixed-Mode Loading Conditions using Cohesive Zone Models YUAN Huang, LI Huan, LI Xiao,Tsinghua University, China (468) 05-04-6 Mechanical behavior and fatigue life assessment of a metastable austenitic stainless steel with severe plastic distortions ZENG Wu, Beijing Institute of Technology, China YUAN Huang, Beijing Institute of Technology, Tsinghua University, China (469) Session5-5 Aeronautical Materials 17:25-18:25 17:25-17:40 05-05-1 Synthesise of Polythioether and Heat Resistant Property of Polythioether Sealants Guo Ruiyi, Zhang Jianzheng, Wu Songhua AVIC Beijing Institute of Aeronautical Materials, China 17:40-17:55 05-05-2 Experimental Investigation of Dynamic properties of AerMet 100 Steel Dayong Hu , Kangpei Meng, Hanlin Jiang Beijing University of Aeronautics and Astronautics, Beijing 100191, P. R. China (248) 05-05-3 Experimental report on the nano-identation testing of textured stainless steel 904 L and 316 L Changjian Geng, Liu Fang, Tong Wenwei, Han Zhenyu, Chi Qingxin AVIC Engine Design And Research Institute, China (13) 17:55-18:10 (173) 18:10-18:25 05-05-4 Microstructure evolution of K6509 cobalt-base superalloy for over-temperature WEI Zhen-wei,ZHAO Wen-xia,ZHOU Jing-yi,LIU Chang-kui,ZHENG Zhen,QU Shiyu,TAO Chun-hu AVIC Beijing Institute of Aeronautical Materials, China AVIC Failure Analysis Center, Beijing 100095, China Beijing Key Laboratory of Aeronautical Materials Testing and Evaluation, China (414) Session6-1 Aircraft Engine System 1 11:00-12:00 06-01-1 Patent analysis of the course of aerojet's business and the key technologies of hypersonic Li Yelan, Bai Yan Zhou Peng Beijing Seahawks Science and Technology Information Institute, China (24) 06-01-2 Support Vector with ROC Optimization Method Based Fuel Consumption Modeling for Civil Aircraft ZHANG Haifeng , Nanjing University of Aeronautics and Astronautics, Nanjing, China Wang Xu-hui , Chen Xin-feng, China Academy of Civil Aviation Science and Technology, Beijing, China (124) 11:30-11:45 06-01-3 Research of Model-based Aeroengine Control System Design Structure and Workflow Dong Zhang, Jin-zhi Lu , Lin Wang , and Jun Li AVIC, Shenyang Engine Design and Research Institute, China (66) 11:45-12:00 06-01-4 Review-Volcanic ash and its influence on aircraft engine components W.R. Chen, AVIC Commercial Aircraft Engine Manufacturing Co., Ltd., ,China L.R. Zhao, National Research Council of Canada, Aerospace, Canada (80) 11:00-11:15 11:15-11:30 Session6-2 Aircraft Engine System 2 13:30-14:30 13:30-13:45 06-02-1 Development Strategy Study for Commercial Aero Engine Companies in European Countries and the United States LIU Hong-xia, ZHANG Shi-fu, LIANG Chun-hua, AVIC Shenyang Engine Design and Research Institute, China LIU Qi, AVIC Academy of Aeronautic Propulsion Technology, China 13:45-14:00 06-02-2 Performance Estimation for Differential Pressurization Pulse Jet Engine Zhang Jianpeng, Qin Lizi, He Miaosheng, Beihang University, China (451) 06-02-3 The Effect of the Inlet Total Pressure and the Number of Detonation Waves on Rotating Detonation Engines Song-Bai Yao, Meng Liu, Jian-Ping Wang Center for Combustion and Propulsion, CAPT and SKLTCS, Peking University, Beijing 100871, China (492) 06-02-4 Research on the Influence of Reflected Shock Wave on Continuously Rotating Detonation Engine Liu Yu-Si, Li Yang, Wang Yu-hui, Wang Jian-ping Centre of Combustion and Propulsion, CAPT & SKLTCS, College of Engineering Peking University, China (494) 06-03-1 Numerical Study of the Combustion Field in Dual-cavity Scramjet Combustor Wang Lu, Qian Zhansen,Gao Liangjie AVIC Aerodynamics Research Institute, China Aviation Key Laboratory of Science and Technology on High Speed and High Reynolds Number Aerodynamic Force Research, China (148) 06-03-2 Atomization Performance Study of a Fuel Injector in IGC by Experimental and Numerical Investigation Can Ruan, Xiaoyuan Fang, Fei Xing, Xiamen University, China Guanxing Huang, Hongzhou Ho, Cleaning Combustion and Energy Utilization Research Center of Fujian Province, JiMei University, China (199) 06-03-3 Effect of combustion heat release on the stability of confined boundary/ mixing-layer confluent flow Liu Zhiyong, , Shang Qing, China Academy of Aerospace and Aerodynamics, China Liu Xiaoyong, Fei Lisen, Liu Fengjun, Beijing Power Machinery Institute, China (239) 14:00-14:15 14:15-14:30 (143) Session6-3 Combustion 1 14:40-15:25 14:40-14:55 14:55-15:10 15:10-15:25 Session6-4 Combustion 2 15:45-17:00 15:45-16:00 06-04-1 Numerical Studies of Multi-cycle acetylene-air Detonation Induced by Shock Focusing Zhihong Zhang, Zhiqiang Li, Gan Dong National National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics, Beijing University of Aeronautics and Astronautics, China 16:00-16:15 06-04-2 Shock tube study on auto-ignition delay of kerosene aerosol and its cracked mixture (401) 06-04-3 The Testing Simulation Technology Investigation on the Thermal Environment of Engine Combustor Wall Material Tu Jianqiang, Chen Lianzhong, Zhang Youhua China Academy of Aerospace Aerodynamics, China (45) 16:15-16:30 16:30-16:45 06-04-4 16:45-17:00 06-04-5 Study on the Ignition System of a Pilot Flame in a Cannon-Type-Combustor of a Turbo-Engine Yasuo Obikane Mongolian University of Science and Technology, Mongolia Experimental Study on Spectral Characteristics of Kerosene Swirl Combustion Hyeonjae Lee, Seonghyeon Seo Hanbat National University, Korea (253) (64) (142) Session6-5 Combustion 3 17:10-18:25 17:10-17:25 06-05-1 17:25-17:40 06-05-2 Study of the Dump Diffuser Optimization for Gas Turbine Combustors Leilei Xu, Yue Huang,Can Ruan, Peiyong Wangand Fei Xing, Xiamen University, China A Large Eddy Simulation Study of Flow and Mixing Characteristics in Supersonic Combustor Kyoo-hwan Moon, Ji-seok Hong, Hong-gye Sung, Korea Aerospace University,, Korea (198) (311) 06-05-3 Analysis of the Flame Structure of Surrogate Kerosene/GOx in Laminar Counterflows JeongSeok Kang, JunYoung Heo, Hong-Gye Sung , Korea Aerospace University, Korea (337) 17:55-18:10 06-05-4 An Experimental Investigation on Combustion Characteristics of Hypermixer Injectors-Effects of the 'Swept' Applied to Hypermixer Injector Ramps-Noritsugu Kubo,, Sadatake Tomioka,Tohoku University, Japan Atsuo Murakami, Kenji Kudo, Kakuda Space Center, Japan Aerospace Exploration Agency, Japan (449) 18:10-18:25 06-05-5 Observation of kerosene injected from a cavity into a supersonic airstream Shengli XU, Liseng FEI Tsinghua University, Institute of Power Machinery, China (400) 07-01-1 The aeroelastic characteristic of a wing with preload asymmetry freeplay Hui Zhang, Jingtao Wu China Aircraft Strength Research Institute, China (249) 07-01-2 Analysis of Fluid-Structure Interaction by High Velocity Impact Hongsu Bae, Kyeongsik Woo, Chungbuk National University, Korea In-Gul Kim, Chungnam National University, Korea Jong-Heon Kim, Agency for Defense Development, Korea (274) 07-01-3 Airfoil Dynamic Stall and Aeroelastic Analysis Based on Multi-Frequency Excitation Using CFD method Daobo huang, Jiandong Li, Yong Liu National Key Laboratory of Rotorcraft Aeromechanics, Nanjing University of Aeronautics and Astronautics, China (392) 07-01-4 Development of Aeroelastic Simulation Code Using Unstructured CFD Solver Hitoshi Arizono Japan Aerospace Exploration Agency, Japan Hamid Reza Kheirandish, Research Center of Computational Mechanics, Inc., Japan (471) 17:40-17:55 Session7-1 Aeroelasticity 11:00-12:00 11:00-11:15 11:15-11:30 11:30-11:45 11:45-12:00 Session7-2 Experimental Techniques and Applications 1 13:30-14:30 13:30-13:45 07-02-1 Experimental estimation on the Running Time of Gun Tunnel Ruiqu Li,, Jian Lin, Xing Chen China Academy of Aerospace Aerodynamics,, China (258) 13:45-14:00 07-02-2 14:00-14:15 07-02-3 14:15-14:30 07-02-4 Experimental Validation on Lift Increment of a Flapping Rotary Wing with Boring-hole Design CHEN Long, YAN Wanfang, WU Jianghao, School of Transportation Science and Engineering, Beihang University, China Dynamic Characteristics of Cryogenic Swirl Flow under Supercritical Conditions Seongho Cho, Haisol Kim, Youngbin Yoon Seoul National University, Korea An Experimental Investigation of Showerhead Film Cooling Performance on a Turbine Blade Zhu Xingdan, Zhang Jingzhou, Tan Xiaoming Jiangsu Province Key Laboratory of Aerospace Power Systems, Nanjing University of Aeronautics and Astronautics, China (260) (262) (292) Session7-3 Experimental Techniques and Applications 2 14:40-15:25 14:40-14:55 07-01-1 14:55-15:10 07-01-2 15:10-15:25 07-01-3 A Wind-Tunnel Study for Drag Characterization of Speed Skating Suits Ki-Hun Lee, In-Ki Kim, Kwang-Soo Kim, Kybeom Kwon Korea Air Force Academy, Korea Young-Jin Moon, Korea Institute of Sports Science, Korea Eun-Mi Choi, Korea Research Institute for Fashion Industry, Korea Oh-Kyung Kwon, BSG Co., Ltd. , Korea Mi-Kyung Kim, DYETEC, Korea Yung-Hwan Byun, Konkuk University, Korea Aeroheating measurement on capsule model with roughness in high-enthalpy shock tunnel HIEST HideyukiTanno,Tomoyuki Komuro, Kazuo Sato, KasuhiroItoh Japan Aerospace Exploration Agency, Japan X3 reflected shock tunnel for extended flow duration R.G. Morgan D.E. Gildfind Centre for Hypersonics, The University of Queensland, Australia (362) (476) (94) Session7-4 Experimental Techniques and Applications 3 15:45-17:00 15:45-16:00 07-04-1 16:00-16:15 07-04-2 16:15-16:30 07-04-3 16:30-16:45 07-04-4 16:45-17:00 07-04-5 New Dynamic Stability Rig for Tri-sonic Wind-Tunnel Liu Jin, Chen Nong, Song Yuhui, Hu Jing, Xie Ke China Academy ofAerospace Aerodynamics,China Improving Quality of Wind Tunnel Test Data Through the MDOE Zhang Jiang ,Ma Handong, Qin Yongming China Academy of Aerospace Aerodynamics, China The Optical Flow Method Research of Particle Image Velocimetry Hong-Wei Wang, Zhan Huang , Jian Gong, Hong-Liang Xiong China Academy of Aerospace Aerodynamics, China Aerodynamic characterization of 'DelFly Micro' in forward flight configuration by force measurements and flow field visualization Shuanghou Deng, Mustafa Percin, Bas van Oudheusden Delft University of Technology, the Netherlands An Experimental Investigation of the Supersonic Planar Mixing Layer with Finite Thickness Hailong Zhang,Jiping Wu,Jian Chen,Weidong Liu Science and Technology on Scramjet Labortatory ,National University of Defense Technology, China (128) (222) (243) (394) (70) Session7-5 Acoustics 17:10-18:25 17:10-17:25 07-05-1 17:25-17:40 07-05-2 17:40-17:55 07-05-3 17:55-18:10 07-05-4 Nonlinear Self-sustained Combustion instability in a Rijke-Zhao Combustor with Three Bifurcating Branches Dan Zhao, S. H. Li, X.Y. Li and C. Z. Ji Nanyang Technological University, Singapore Passive Control of Self-sustained Combustion Oscillations Using Electrical Heaters in a T-shaped Thermoacoustic System Dan Zhao, S. H. Li, X. Y. Li, C. Z. Ji Nanyang Technological Universtiy, Singapore Azimuthal instabilities in annular Chambers with flow and axial distributed heat source Lei Li, Dan Zhao, Nanyang Technological University, Singapore Xiaofeng Beijing University of Aeronautics and Astronautics, China A combined shape and liner optimization of a general Aero-engine Intake for tone noise reduction S Qiu, J Y Ying Dept. of Discipline Engineering, AVIC Commercial Aircraft Engine CO.LTD, No.3998 South Lianhua Road, Shanghai, 201108, China (95) (97) (146) (151) 18:10-18:25 07-05-5 A frequency domain Immersed Boundary method and its application to 2-dimensional acoustic problems A. Liang AVIC Commercial Aircraft Engine co. ltd., China (214) Session8-1 Flight Mechanics 1 11:00-12:00 11:00-11:15 08-01-1 11:15-11:30 08-01-2 11:30-11:45 08-01-3 11:45-12:00 08-01-4 Experimental Study on Aerodynamic Characteristics of Ornithopter Hiroki T Endo Kyushu Sangyo University, Japan, Hironori A. Fujii Kanagawa Institute of Technology, Japan A Study on the Trajectory Optimization of a Tiltrotor with the Tilting Rate Limit Takahide Miyamoto,Hiroyuki Takano, Isao Yamaguchi and Takeshi Yamasaki National Defense Academy, Japan A New Minimum Infinity-Norm Solution: with Applications to Spacecraft Attitude Controls Hyungjoo Yoon, Hyun Ho Seo, Young-Woong Park, Hong-Taek Choi Korea Aerospace Research Institute, Korea Analysis of Non-uniform Inflow Models and Parameter Estimation of an Unmanned Coaxial Rotor Helicopter in Forward Flight Mohammad Harun-Or-Rashid, Jun-Beon Song, Young-Seop Byun, Beom Soo Kang Pusan National University, Korea (74) (75) (110) (113) Session8-2 Air Traffic Management 1 13:30-14:30 13:30-13:45 08-02-1 13:45-14:00 08-02-2 14:00-14:15 08-02-3 14:15-14:30 08-02-4 Research on the MOIPSO Model for Collaborative Capability-flow Allocation in Multi-airports Terminal Area Chen Hao, Wu Yi, Wang Zhan, Nanjing University of Aeronautics and Astronautics, China A Agent-based Approach to Automated Merge 4D Arrival Trajectories in Busy Terminal Maneuvering Area LIANG Man, Nanjing University of Aeronautics and Astronautics, China Real Time Image Haze Removal on Multi-core DSP Linting Bai, Yongwei Wu, Dep. of Computer Science & Technology, No.1, Tsinghua Yuan, China Jianchun Xie, Pengcheng Wen AVIC Computing Technique Research Institute, China Aviation Key Laboratory of Science and Technology on Airborne and Missileborne Computer, China Constructing an Index of Difficulty for Air Traffic Control Using Proximity Parameters Sakae Nagaoka, Mark Brown ATM Department, Electronic Navigation Research Institute, Tokyo (34) (81) (99) (310) Session8-3 Air Traffic Management 2 14:40-15:25 14:40-14:55 14:55-15:10 15:10-15:25 08-03-1 Optimization of Approach Trajectory Considering the Constraints Imposed on Flight Procedure Design Tomoki Hasegawa, Takeshi Tsuchiya, The University of Tokyo, Japan Ryota Mori Electronic Navigation Research Institute, 7-42-23 Jindaiji-higashi-machi, Chofu, Tokyo, 182-0012, Japan (452) 08-03-2 Reducing Fuel Burn through Air Traffic Flow Optimisation Incorporating Wind Models Zena Assaad, Cees Bil, Andrew Eberhard, Matthew Moore1 RMIT University, AUSTRALIA (461) 08-03-3 Study on Key Techniques of Aeronautical Ad Hoc Network MAC and Network Layer Qiming Qiu, Cheng Gong China National Aeronautical Radio Electronics Research Institute, China; Zheng Fang Shanghai Jiao Tong University,, China. (463) Session8-4 Guidance Control 15:45-16:30 15:45-16:00 08-04-1 Design of Optimal Earth-Moon Transfer Trajectory via L1 Point Using Energy Level Shaping Method Jin Haeng Choi, Tae Soo No, Gyeong Eon Jeon Department of Aerospace Engineering Chonbuk National University, Korea (408) 16:00-16:15 16:15-16:30 08-04-2 Analysis of Lunar Lander's Necessary Thrust Force in Landing Phase. (431) 08-04-3 Investigation of Estimation Methods for the Time-Varying Residual Magnetic Moment Halil Ersin Soken, Shin-ichiro Sakai Japan Aerospace Exploration Agency (JAXA) Institute of Space and Astronautical Science (ISAS), Japan (433) 08-05-1 Hybrid Re-entry Guidance for Reusable Launch Vehicle Wang Zhi, Zhang Ran, Li Huifeng Beijing University of Aeronautics and Astronautics, China (105) 08-05-2 Mars Atmospheric Entry Guidance Design by Sliding Mode Disturbance Observer-Based Control Yue-Chen Huang, Hai-Yang Li, Jin Zhang, Xin Du National University of Defense Technology, China (251) 08-06-1 A Long-Term Analysis of the GPS Boradcast Orbit and Clock Error Variations Mingyu Kim, Jeongrae Kim, Korea Aerospace University, Korea (332) 08-06-2 Efficient Alignment of Position Measurements with Differing Reference Frames ChrisRAABE, NiklasBERGSTR?M,, MatoshiISHIKAWA, ShinjiSUZUKI The University of Tokyo, Japan EmadSAAD, JohnVIAN Boeing Research and Technology, The Boeing Company, Seattle, USA (364) 08-06-3 Trajectory Optimization Analysis by Dynamic Programming for Operational Feasibility Study of Supersonic Transport Akinori Harada, Yoshikazu Miyazawab, Kyushu University, Japan Atsushi Ueno, Yasushi Watanabe Japan Aerospace Exploration Agency, Mitaka, Japan (399) Session8-5 Guidance Technology 16:30-17:00 16:30-16:45 16:45-17:00 Session8-6 Control Theory and Analysis 17:10-17:55 17:10-17:25 17:25-17:40 17:40-17:55 Session8-7 Flight Quality, Fault Diagnosis and Tolerant Control 17:55-18:25 17:55-18:10 08-07-1 Flight evaluation of fault-tolerant control system using simple adaptive control method Daichi Tokunaga, Shinji Suzuki, The University of Tokyo, Japan Kazuya Masui, Japan Aerospace Exploration Agency, Japan 18:10-18:25 08-07-2 Application Research of MRAC in Fault-Tolerant Flight Controller Shuguang ZHANG, Yang Feng, Di Zhang BeiHang University XueYuan Road No.37, Beijing, 100191, China (209) (457) Parallel Session Schedule DAY2 Session 1-6 Aircraft Aerodynamics 1 13:30-14:30 13:30-13:45 01-06-1 Study of Aerodynamic Configuration Design and Wind Tunnel Test for Solar Powered Buoyancy-lifting Vehicle in the Near-space Guangqiang Chen, Bingyan Chen, Pengfei Li, Peng Bai, Chunqun Ji The Institute of aerodynamics theories and application of China Academy of Aerodynamic of Aerospace (CAAA), China 13:45-14:00 01-06-2 Aerodynamic Configuration Design of Flight Demonstrator for Real Gas Effect Chen Bingyana, Liu Zhoua, Gong Anlong China Academy of Aerospace Aerodynamics, China (155) 01-06-3 The aerodynamic characteristics of micro quadrotor in hovering near walls Yuya Yokoyamaa, Daiki Tsujia,Satoshi Kataokaa, Yuta Chonoa, Ayaka Yashimaa, Mizue Munekataa, Hiroyuki Yoshikawa Kumamoto University, Japan (279) 01-06-04 Effects of the rotor blade interval on the flow field around a quad-rotor in hovering Daiki Tsujia, Yuya Yokoyamaa, Yuta Chonoa, Mizue Munekataa, Hiroyuki Yoshikawa Kumamoto University, Japan (281) 01-07-1 Numerical investigation of configuration influence on propeller-induced noise Minwoo Kim, Youngmin Park, and Yongwun Jung Korea Aerospace Research Institute, Korea (291) 01-07-2 Effect of Close-Coupled Canards on Longitudinal Aerodynamic Characteristics of a Supersonic Configuration Zhong Lei, Keisuke Takizawaa, Tokyo University of Science, Japan Dongyoun Kwakb, Masayoshi Noguchib, Institute of Aeronautical Technology, JapanAerospace Exploration Agency, Japan (450) 15:10-15:25 01-07-3 Reynolds Number Effect on Vortex Dominant Flow of the SST Configurations Dongyoun Kwaka, Japan Aerospace Exploration Agency, Japan Keisuke Ohirab, Ryoyu Systems Co., Japan Ralf Rudnik, German Aerospace Center, Germany (472) 15:25-15:40 01-07-4 The Numerical Simulation of Civil Transportation High-lift Configuration Hao Xuan, Su Cheng, Hu Ning, Zhang weimin China Academy of Aerospace Aerodynamics, China (21) 01-08-1 Special Feature of longitudinal stability and control transporting short takeoff and landing airplane with method increasing lift force Tran The Hunga, Nguyen Quoc An Le Quy Don Technical University, Vietnam (116) 01-08-2 Aerodynamic Interference Caused by the Inboard Leading-Edge Flap on the Outboard Area of the Cranked Arrow Wing Kosuke TOYODA, Kenichi RINOIE The University of Tokyo, JAPAN Dongyoun KWAK, Masayoshi NOGUCHI, Japan Aerospace Exploration Agency, JAPAN (137) 01-08-3 Kriging-algorithm-based Aerodynamic Model for Flush Airdata System Yibin WANG, Xueqiang LIU, Nanjing University of Aeronautics and Astronautics, China Ning QIN, The University of Sheffield, UK (144) 01-09-1 System Dynamics Based Simulation Approach on Corrective Maintenance Cost of Aviation Equipments Liu Fang, Huang Zhaodong Aviation Industry Development Research Center of China, China Lianbo ZHANG, School of Astronautics, Beijing University of Aeronautics and Astronautics, China (241) 01-09-2 Development and Production Costs Estimating For Aviation Equipment Based on Uncertainty Design Huang Zhaodong, Luo Rongxuana, Aviation Industry Development Research Center of China, China Jin Jing, AVIC Chengdu CAIC Electronics co.,LTD, China (240) 14:00-14:15 14:15-14:30 (10) Session 1-7 Aircraft Aerodynamics 2 14:40-15:40 14:40-14:55 14:55-15:10 Session 1-8 Aircraft Aerodynamics 3 16:00-16:45 16:00-16:15 16:15-16:30 16:30-16:45 Session 1-9 Cost Engineering 16:55-17:25 16:55-17:10 17:10-17:25 Session 1-10 Cooling System 17:25-18:10 17:25-17:40 17:40-17:55 17:55-18:10 01-10-1 Simulation Study of Cooling System Temperature Control Based on subsection control WANG Jiali, Li Yanna AVIC The First Aircraft Institute, China (57) 01-10-2 Experimental investigation on flow characteristics of gaseous in microchannels Zhang Kai, Zheng Guanghua, Du Fenglei Northwestern Polytechnical University, Xi'an, China (421) 01-10-3 Numerical Simulation and Thermal Analysis of Stratospheric Airship Kangwen Sun, Qinzhen Yang, Yong Xie, Mou Sun, Xiaoming Chen, Beihang University Yang Yang, Shun Wang, China Aerospace Science and Technology Corporation the Eighth Academy 811 institute, Shanghai, China (455) Session 2-6 New Methods of Navigation, Estimate and Tracking 13:30-14:30 13:30-13:45 02-06-1 13:45-14:00 02-06-2 14:00-14:15 02-06-3 14:15-14:30 02-06-4 Maneuver strategy Adaptive Target Tracking Algorithm by Integrated Kalman Information Filtering Ying LI, Deyun ZHOU, Hao ZHANG, Northwestern Polytechnical University, China A Comparison Study of Advanced Tracking Differentiator Design Techniques Wang Hongwei, Wang Heping, Northwestern Polytechnical University, China Glide Path Angle Tracking Control for UAV Automatic Carrier Landing Seokwon Lee, Hyunjin Choi, Youdan Kim, Sungwan Kimb, Seoul National University, Korea Jinyoung Suk, Seungkeun Kim, Chungnam National University, Daejeon, Republic of Korea Multilateration System Network for Locating Aircraft in a Terminal Control Area Sanghoon Jo, Sangho Ko, Jay Kang Korea Aerospace University, Korea. (42) (109) (175) (275) Session 2-7 GNC of Miniature Aircraft 14:40-15:40 02-07-1 L1 Adaptive Dynamic Inversion Controller for an X-Wing Tail-Sitter MAV in Hover Flight Wang Jin,Song Bifeng, Wang Liguang, Tang Wei, Northwestern Polytechnical University, China (46) 14:55-15:10 02-07-2 Development of Large-Scale 3D Map Generation System for Indoor Autonomous Navigation Flight - work in progress SungTae Moon, Wesub Eom, Hyunchul Gong, Korea Aerospace Research Institute, Korea (293) 15:10-15:25 02-07-3 Control Strategy of Transition Flight Using MPC for QTW-UAV Ryota Hatori, Kenji Uchiyama, Nihon University, Japan (437) 15:25-15:40 02-07-4 Fast SLAM for MAV Using Relative Position Measurements Ryosuke Fujiwara, Takeshi Tsuchiya, The University of Tokyo, Japan Daisuke Kubo, JAXA, Japan (447) 14:40-14:55 Session 2-8 GNC of Spacecraft 16:00-17:30 02-08-1 Orbit Determination of Korea Regional Navigation Satellite System Using InterSatellite Links and Ground Observations Jungmin Choi, Chandeok Park, Sang-Young Park, Yonsei University,, Korea (71) 16:15-16:30 02-08-2 Boost-phase Missile Autopilot Design Based on SDRE with Adaptive Neural Networks Jaeho Lee, Youkyung Hong, Yongwoo Lee, Youdan Kim, Department of Mechanical and Aerospace Engineering, Seoul National University, Korea Gwanyoung Moon, Byung-Eu Jun, Agency for Defense Development, Korea (172) 16:30-16:45 02-08-3 The Ascent Trajectory Optimization of Two-Stage-To-Orbit Aerospace Plane Based on Pseudospectral Method Jing Songa, Haoqin Su, China Academy of Aerospace Aerodynamic, China (231) 16:45-17:00 02-08-4 Suboptimal Formation Reconfiguration of Satellites Under Input Directional Constraints Yasuhiro Yoshimura, Tokyo Metropolitan University, Japan (246) 16:00-16:15 17:00-17:15 17:15-17:30 02-08-5 FUEL-OPTIMAL IMPULSIVE SATELLITE FORMATION RECONFIGURATION WITH IMPROVED SEMI-ANALYTICAL GLOBAL SEARCH ALGORITHM Youngkwang Kim, Sang-Young Park, Yonsei University, Korea (202) 02-08-6 Recent Developments of Experimental Winged Rocket: Autonomous Guidance and Control Demonstration Using Parafoil G.Guna Surendra, K.Yonemoto, T.Matsumoto, Y.Kutsuna, K. Itakura, H. Yamasaki, Y.Ura, M.Ichigie, Kyushu Institute of Technology, Japan H.Tanaka, S.Ueno, T. Someya, IHI Aerospace Co., Ltd. Japan (304) Session 2-9 Target Identification Technique 17:40-18:10 17:40-17:55 02-09-1 A Collision Avoidance System using a LIDAR Sensor Jingu Kim, Sua Song, Inhyun Kim, Seungkeun Kim and Jinyoung Suk, Chungnam National University, Korea (272) 17:55-18:10 02-09-2 Automatic Target Recognition with semi-supervised Learning in Aerial Images Chanho Kim, Hyochoong Bang, Korea Advanced Institute of Science and Technology, Daejeon, Korea (375) Session 3-6 CFD Applications 1 13:30-14:30 13:30-13:45 03-06-1 13:45-14:00 03-06-2 14:00-14:15 03-06-3 14:15 -14:30 03-06-4 Study On The Vortex Shedding Mechanism Of Coupling Combustion Stabilizer With V-gutter and Strong Swirl Flow Gan Dong, Zhiqiang Li and Zhihong Zhang, National Key Laboratory of Science and Technology on Aero-Engine Aerothermodynamics, Beijing University of Aeronautics and Astronautics, China Applying CFD Technology to Determine the Effect of Two New Designed Fan Inlet Distortion Generators Li Zhipeng, Lu Chao, Wu Hui, Liu Xiaopeng, Zhang Guowang, AVIC Shenyang Engine Design and Research Institute, China Transition Prediction for Three-Dimensional Configurations Using a Transition Transport Model Considering Crossflow Effect Jeong Hwan Sa, Sang Eon Jeon, Soo Hyung Park, Konkun University, Korea Kyung Jin Jung, Agency for Defense Development, Korea Flow Characteristics of 2-dimensional Supersonic Nozzle According to Nozzle Pressure Ratio Hyun Ah Choi, Seong Hun Bae, Jeong Soo Kim, Pukyong National University, Korea (267) (294) (329) (429) Session 3-7 CFD Applications 2 14:40-15:55 14:40-14:55 03-07-1 14:55-15:10 03-07-2 15:10-15:25 03-07-3 15:25-15:40 15:40-15:55 Numerical simulation study on propeller slipstream interference of high altitude long endurance unmanned air vehicle Guangqiang,Chen Bingyan,Chen Pengfei, Li Peng Bai,Chuqun Ji, China Academy of Aerodynamic of Aerospace (CAAA), China Simulation of rain effects on aerodynamic performance of an airfoil ZHANG Rui-min, China Academy of Aerospace Aerodynamics, China A CFD based sonic boom prediction method and investigation on the parameters affecting the sonic boom signature Lengyan Qian Zhansen AVIC Aerodynamics Research Institude, China Aviation Key Laboratory of Science and Technology on High Speed and High Reynolds Number Aerodynamic Force Research, China (11) (43) (119) 03-07-4 Applications of Overset Grid Technique to CFD Simulation of High Mach Number Multi-body Interaction/Separation Flow Li Xuefei,Liu Yuan,Qian Zhansen AVIC Aerodynamics Research Institude, China Aviation Key Laboratory of Science and Technology on High Speed and High Reynolds Number Aerodynamic Force Research, Shenyang, China (125) 03-07-5 Investigation on Different Methods for Numerical Simulation of Propeller Slipstream Zhang Ying, Ye Liang, Yang Shuo, Zhu Xinglin Chinese Aerodynamic Research Institute on Aeronautics, China (156) Session 3-8 Simulation of Unsteady Aerodynamics 16:05-17:20 16:05-16:20 03-08-1 Investigation of Airfoil Unsteady Aerodynamic Characteristics Based on Finite Macro-Element and TFI Hybrid Dynamic Mesh Correction TANG Han, GAO Zhenxun National Laboratory of Computatioal Fluid Dynamics, Beihang University, China (53) 03-08-2 Numerical Simulation of Unsteady Separated Flow over a Delta Wing Using Cartesian Grids and DES/DDES Meng Lv, Shuai Fang, Yudong Zhang China Academy of Aerospace Aerodynamics, China (102) 16:35-16:50 03-08-3 High-Performance Computing of Periodic Unsteady Flow Based on Time Spectral Method XIE Lijun, YANG Yunjun, LIU Zhou, ZHOU Weijiang China Academy of Aerospace Aerodynamics, China (159) 16:50-17:05 03-08-4 Unsteady Flow Numerical Simulation of Vertical Axis Wind Turbine Du Gang, Wu Chun Kau BeiHang University, China (453) 03-08-5 Coherence Mapping of Unsteady Pressure Fields on 2-Dimensional Wings Using Unsteady Pressure-Sensitive Paint Technique Kazuyuki Nakakita Japan Aerospace Exploration Agency (JAXA), Japan. (478) 16:20-16:35 17:05-17:20 Session 3-9 Simulation of Aerodynamic Heating 17:30-18:15 17:30-17:45 03-09-1 17:45-18:00 03-09-2 18:00-18:15 03-09-3 Effects of Nose and Corner Radius on Heat Transfer Rates over Axisymmetric Blunt Body Zhang Liang,Chen Zhi,Gong Jian,Zhang Xuejun China Academy of Aerospace Aerodynamics, China Study on the unsteady aerodynamic heating of the oscillating model Hu Peng-ju, Zhang Liang,Zheng Jin-xin China Academy of Aerospace Aerodynamics, China Study on Correlation of Aerodynamic Heating Data of a Combination Model SHA Xin-guo, CHEN Xing, JI Feng, SU Peng-hui China Academy of Aerospace Aerodynamics, China (104) (131) (192) Session 5-6 Flight Mechanics 3 13:30-14:30 13:30-13:45 05-06-1 13:45-14:00 05-06-2 14:00-14:15 05-06-3 14:15-14:30 05-06-4 Aerodynamic Characteristics and Flight Capability Prediction of the Smallscale Flight Experiment Vehicle Being Developed at Muroran Institute of Technology, Japan Satoshi Kondo, Yoshihiro Suzuki, Kazuhide Mizobata, Ryojiro Minato, Kazuyuki Higashino,Nobuhiro Tanatsugu, Muroran Institute of Technology,, Japan Aerodynamic force measurement and flow visualization for flapping micro aerial vehicle Tatsuya Nomura, Yuuta Torii, Aichi Institute of Technology, Japan Shigeru Obayashi, Yasuhumi Konishi Tohoku University, Japan Optimal Ascending Trajectory Design of High Altitude Long Endurance UAVs Using Wind Modeling Kiduck Kim, Yunju Na, Hyochoong Bang Korea Advanced Institute of Science Technology, Korea Donghun Lee, Hyoungsik Choi Korea Aerospace Research Institute, Korea Sangjong Lee Inha Technical Collage, Korea Three Dimensional Trajectory Linearization Control for Flight of Air-breathing Hypersonic Vehicle G. D. Zhu, Z. J. Shen Beijing University of Aeronautics and Astronautics, China (270) (333) (359) (464) Session 5-7 Aeronautical Structural Manufacture and Test 14:40-16:10 14:40-14:55 05-07-1 14:55-15:10 05-07-2 15:10 -15:25 05-07-3 The Application Research of ID Chip for Strain Measurement in Full Scale Aircraft Structure Strength Static Test Jia Zuo, Gang Wang Full scale aircraft static/fatigue structure aviation science and technology key laboratory, Aircraft Strength Research Institute of China, China Research of weight deduction in full-scale aircraft static strength test Liu bing, Zhang lei, Xia feng Key Laboratory of static and fatigue test of full scale aircraft, AVIC Aircraft Strength Research Institute, China A Method for modify the Thermal Stress in the Wind Tunnel Wang Ying, Wang Wei, Bu Junhui, Chen Ding China Academy of Aerospace Aerodynamics, China (134) (174) (229) 15:25-15:40 15:40-15:55 15:55-16:10 05-07-4 Fatigue Testing and Analysis of Aircraft Structure Subjected to Aerodynamic and Buffet Loads Li Yixuan, Zhang Zhijun, Shao Chuang Laboratory of Aeronautical Acoustics and Dynamics, Aircraft Strength Research Institute, China (355) 05-07-5 Landing Gear Ground Load Measurement and Verification Test for a Large Passenger Jet Kong Xiangjun, Le Ningning, Li Chunsheng, Xiao Xianbo, Lin Bo, Xu Bing China Academy of Civil Aviation Science and Technology, China (107) 05-07-6 U-shaped bolts fracture failure analysis Huanping Kong, Delin LIU, Tao JIANG AVIC Beijing Institute of Aeronautical Materials, China AVIC Testing Innovation Cooperation, China Beijing Key Laboratory of Aeronautical Materials Testing and Evaluation, China (415) Session 5-8 Structural Dynamics and Aerodynamics 16:30-17:00 16:30-16:45 16:45-17:00 05-08-1 Static and Free Vibration Analysis of Cylindrical Shells with Shear and Normal Deformations Effects Ngoc Doan Tran, Le Quy Don Technical University, Vietnam Anh Tuan Nguyen Le Quy Don Technical University, Vietnam, KAIST, Korea (391) 05-08-2 An Approximate Method of a Composite Plate's Modal Analysis using Modified Spatial Function Yongha Kim, Myungjun Kim, Sangbong Lee, Kyungmin Hwang, Graduate School of Korea Aerospace University, Korea Jungjin Lee, Korea Aerospace Research Institute, Korea Jungsun Park School of Aerospace and Mechanical Engineering, Korea Aerospace University, Korea (491) Session 5-9 Jet Flows 17:00-17:45 17:00-17:15 05-09-1 17:15-17:30 05-09-2 17:30-17:45 05-09-3 Oscillation flow induced by underwater supersonic gas jets from a rectangular Laval nozzle He Miaosheng, Qin Lizi, Liu Yu Beijing University of Aeronautics and Astronautics, China Fluid-particle Interaction and Particle Distribution in a Particle-laden Coaxial jet Jungsoo Yoon, Youngbin Yoon Seoul National University, Korea Development of Aerodynamic Design of Hypersonic Quiet Nozzles Ruiqu Li, Junmou Shen, Jian Gong China Academy of Aerospace Aerodynamics, China (245) (247) (256) Session 5-10 Composite Materials 17:55-18:40 17:55-18:10 05-10-1 18:10-18:25 05-10-2 18:25-18:40 05-10-2 Vibration Reduction of a Bearingless Helicopter Rotor with Composite Tailored Couplings YU Jin, LUO Yu, LIU Yong, Nanjing University of Aeronautics and Astronautics, China Viscoelastic Behaviors of Shape Memory Polymer Composites O-Hyun Kwon, Hark-Inn Kim, Soo-Yong Lee, Jin-Ho Roh Korea Aerospace University, Korea Kyo-Nam Koo University of Ulsan, Korea Prediction of Distortion in Flanged Composite Laminates Using Viscoelastic Models Xiao Lin Liu, Paul Falzon Advanced Composite Structures Australia Pty Ltd, Australia (170) (296) (485) Session 6-6 Turbine and Heat Trasnfer 13:30-14:30 13:30-13:45 13:45 -14:00 06-06-1 Evolution of Rolls-Royce air-cooled turbine blades and feature analysis LI Xu, SUN BO, YOU Hongde, WANG Lei AVIC Shenyang Engine Design and Research Institute, China (76) 06-06-2 Design Optimization of Profiled Endwall in a High Pressure Turbine Rotor Including Rim Seal Purge Flow Effects Hualing Luo, Huimin Tang, Shuzhen Hu, Shuaiqiang Liu AVIC Commercial Aircraft Engine Co., LTD., China (153) 14:00 -14:15 06-06-3 14:15-14:30 06-06-4 Study of the Pressure Drop and Thermal Performance of An Air-Air Heat Exchanger for Aero-Engine Application Lu Haiying, Lv Duo, Li Yi, Shen Yi AVIC Shenyang Aero-engine Research Institute, China Yu Xiao, AVIC Shenyang Aero-engine Research Institute, China National Key Laboratory on Aero-engines, Beijing University of Aeronautics and Astronautics, China Dong Wei Shanghai Jiao Tong University, China Conjugate Heat Transfer Simulation of a Thermal Barrier Coated Turbine Vane Jinuk Kim, Jeonggyu Bak, Jinsoo Cho Hanyang University, Korea Youngseok Kang, Korea Aerospace Research Institure, Korea (149) (197) Session 6-7 Spacecraft Propulsion System 14:40-16:10 14:40-14:55 06-07-1 Orbit Design for Approaching Multiple Space Objects in a Circular Orbit WEI Yanyan, WANG Hongyu, Army Aviation Institute, China LV Zhaofu, 65529Army, China 14:55 -15:10 06-07-2 Study on algorithms of flush air data sensing system for hypersonic vehicle Guangqiang Chen,Guidong Wang,Bingyan Chen,Weijiang Zhou,Chuqun Ji China Academy of Aerodynamic of Aerospace (CAAA), China (12) 15:10-15:25 06-07-3 Nine-degree of Freedom Modeling and Flight Dynamic Analysis of Parafoil Aerial Delivery System Yu Gang 29# Xinhua Road, Xiangyang City, Hubei Province, China (38) 15:25-15:40 06-07-4 Morphing process research of UAV with PID controller Su Haoqin, Bao Xiaoxiang, Shi Hongwei, Song Jing, Huang Zhan, The 2nd Department of China Academy of Aerospace Aerodynamic, China (58) 15:40-15:55 06-07-5 The Effect of Airflow over Mountains on Flight Safety Chen Junping,,Wang Lixin Beijing University of Aeronautics and Astronautics, China (211) 06-07-6 Assessment of Landing Gear Design based on the Virtual Testing and Evaluation Methodology Liu Hailiang, Wang Lixin, Beijing University of Aeronautics and Astronautics, China (298) 15:55-16:10 (6) Session 6-8 Spacecraft Propulsion System 1 16:30-17:30 06-08-1 Optimization Selection of Regulated Pressurization System Schemes for Liquid Attitude and Divert Propulsion Systems Lie LIU, Guo-zhu LIANG Beihang University, China (181) 06-08-2 Investigation on effective sampling strategy for multi-objective design optimization of RBCC propulsion systems via surrogate-assisted evolutionary algorithms Tuan Quang Ho, Hideaki Ogawa, Cees Bil RMIT University, Australia (219) 17:00-17:15 06-08-3 Potential of ADN-based ionic liquid propellant for spacecraft propulsion Yuichiro Ide School of Physical Sciences,Department of Space and Astronautical Science, The Graduate University for Advanced Studies, Japan Takuya Takahashi, Keiichiro Iwai, Japan Carlit Co., Ltd., Japan Katsuhiko Nozoe Carlit Holdings Co., Ltd., Japan Hiroto Habu, Shinichiro Tokudome Japan Aerospace Exploration Agency (JAXA), Japan (343) 17:15-17:30 06-08-4 Structural Damping Effect on Deformation of Flexible Flapping Wing Xue Dong, Song Bifeng, Yang Wenqing, Fu Peng Northwestern Polytechnical University, Xi'an, P.R. China (115) 16:30-16:45 16:45-17:00 Session 6-9 Spacecraft Propulsion System 2 17:40-18:40 17:40-17:55 06-09-1 Experimental Studies on AeroThermodynamic Environments of the Interaction Area between the Wing and the Arc Board in Arc Wind Tunnel XU Kao, CHEN Lianzhong, LIU Xiang China Academy of Aerospace Aerodynamics, Beijing (233) 17:55-18:10 06-09-2 18:10-18:25 06-09-3 18:25-18:40 06-09-4 Technology and Application of Identifying Dynamic Loads Based on Flight Test Data Chen Liebin, Jin Wei, Shi Shanglu Chengdu Aircraft Design and Research Institute, China Plume interference effects on cluster operations of Hall thruster system Yudai Uyama, Takeshi Miyasaka, Katsuo Asato, Daiki Furutaa, Daichi Shimizua, Ryota Gotoa, Mikoto Yoshidaa, Ryosuke Murakia Gifu University, Japan Mixing Enhancement in a RBCC Engine Operating in Hypersonic Flow Ryosuke Nakano, Noritsugu Kubo JAXA Kakuda Space Center, Japan Sadatake Tomioka, Atsuro Murakamib, Kenji Kudob, Shuichi Uedab Tohoku University, Sendai, Japan (16) (493) (114) Session 7-6 Conceptual Design and Evaluation Methods 13:30-14:30 13:30-13:45 07-06-1 13:45-14:00 07-06-2 14:00-14:15 07-06-3 14:15-14:30 07-06-4 System Design of Solar Sail Deployment and its Effect on Attitude dynamics for Cube Satellite CNUSAIL-1 Su-A Song, Yeona Yoo, Chang-Gu Han, Soyeon Koo, Jinyoung Suk, Seungkeun Kim Chungnam National University, Daejeon, Republic of Korea Surrogate Model of Aerodynamic Model toward Efficient Digital Flight Norazila Othman, Masahiro Kanazaki Tokyo Metropolitan University, Japan Improved Flight Load Analysis for Light Aircraftby Using Multi-Fidelity Database Seung-Bin Park, Nhu Van Nguyen, Sangho Kim, Jae-Woo Lee Department of Aerospace Information Engineering Konkuk University, Korea, Aircraft Structural Sizing and Weight Estimation Using FE-based Preliminary Design Tool Danbi Hong,, Wanggu Kang, Hae-Chang Lee, Dae Sung Lee, Korea Aerospace Reasearch Institute, Korea Seung Jo Kimb Seoul National University, Korea (305) (416) (448) (350) Session 7-7 Fluid -Structure Coupling 14:40-16:10 14:40-14:55 07-07-1 14:55-15:10 07-07-2 15:10-15:25 07-07-3 15:25-15:40 07-07-4 15:40-15:55 07-07-5 15:55-16:10 07-07-6 Numerical Research on Segmented flexible airfoils considering fluid-structure interaction DONG Hefeng,WANG Chenxi,LI Shaobin,SONG Xi Zhen National Key Laboratory on Aero-Engines, Beihang University., China Study on Two-dimensional Wing Flutter Analysis by a High-order Flux Reconstruction Method Issei Morinaka, Koji Miyaji Yokohama National University, Japan Sensitive Flutter Parameters Analysis with Respect to Flutter-Free Design of Compressor Blade Sun Hai, Yang Lin, Li Hongxin AVIC Shenyang Engine Design and Research Institute, Shenyang, China Body freedom flutter of a blended wing body model coupled with flight control system Yingsong Gu, Zhichun Yang, Shun He Institute of Structural Dynamics and Control, Northwestern Polytechnical University, China Surface recombination effects on surface friction of reentry vehicles Miao wenbo, Huang fei, Zhang liang, Cheng xiaoli China Academy of Aerospace and Aerodynamics,China Aerodynamic Performance of Micro Flexible Flapping Wing by Numerical Simulation Yang Wenqing, Wang Liguang, Xue Dong, Song Bifeng Northwestern Polytechnical University, China (445) (182) (189) (194) (244) ( ) Session 7-8 Flow Control 1 16:30-17:30 16:30-16:45 07-08-1 16:45-17:00 07-08-2 Investigation active flow to control the separation over an airfoil NACA 2415 Tran The Hung, Nguyen Minh Xuan Le Quy Don Technical University, Vietnam A Numerical investigation of the Sparkjet Actuator in Multiple-shot Mode LV Yuan-wei, SHAN Yong, ZHANG Jing-zhou, TAN Xiao-ming Jiangsu Province Key Laboratory of Aerospace Power Systems, Nanjing University of Aeronautics and Astronautics, China (86) (158) 17:00-17:15 07-08-3 17:15-17:30 07-08-4 Prediction of Projectile Trajectories Launched from Helicopter Hyojoon Gong, Seungsoo Lee Inha University, Korea Jae Seong Park Agency for Defense Development, Korea Numerical Study of Active Flow Control on a Vertical Tail Shangze Li, Zhao Li, Haixin Chen and Yufei Zhang Tsinghua University, Beijing, 100084, China (264) (284) Session 7-9 Flow Control 2 17:40-18:40 Simulation of Unsteady Flow Actuation Produced by Surface Plasma Actuator on 2-D Airfoil Phan Minh Khang. E-vehicle Institute, University of Ulsan, Ulsan, Korea Jichul Shin Department of Aerospace Engineering, University of Ulsan, Korea Investigation onSpanwise Wall Oscillation in Turbulent ChannelFlow Based on Reynolds Stress Model (RSM) DUAN Dehao, ZHANG Jinbai, GAO Zhenxun National Laboratory of Computational Fluid Dynamics, Beihang University, China 17:40-17:55 07-09-1 17:55-18:10 07-09-2 18:10-18:25 07-09-3 Modeling of the Heat Interface of a Plasma Actuator Yasuo Obikane, Khemedekh Lochin Mongolian University of Science and Technology, Mongolia (204) 07-09-4 Improvement of Deformation Measurement Performance of the SPR Camera System using SPR Interactive Modeling and Simulation Framework Jong-Min Yun, Hong-Il Kima, Jae-Hung Han Department of Aerospace Engineering, KAIST, Korea Hyuk-Jun Kwon Agency for Defense Development, Korea (250) 18:25-18:40 (302) (377) Session 8-8 Aerodynamic Studies of Power Systems 1 13:30-14:30 13:30-13:45 07-10-1 13:45-14:00 07-10-2 14:00-14:15 07-10-3 14:15-14:30 07-10-4 Numerical Study of the Leakage Flow on a Novel Turbine Blade Tip Dengyu Jianga, Hualing Luoa, Xiang Zhanga AVIC Commercial Aircraft Engine Co., LTD., China The Aerodynamic Design and Investigation of Loading Distribution of a Mixed Flow Compressor Chen Xuanyu,, Gui Xingmin, Jin Donghai Beihang University, China Meng Xiangwei China Aero-polytechlonogy Establishment, China Influence of Geometric Scaling on Linear Cascade Aerodynamic Performance Chen Fen-fen, Gui Xing-min, Jin Dong-hai, Qiu Dao-bin Beihang University,China Study on the design of supersonic axisymmetric multicompression and quasiisentropic inlets JIANG Yun-song, GAO Zhen-xun, JIANG Chong-wen Beihang University, Beijing, 100191, China (93) (130) (136) (168) Session 8-9 Aerodynamic Studies of Power Systems 2 14:40-16:10 14:40-14:55 07-11-1 14:55-15:10 07-11-2 15:10-15:25 07-11-3 15:25-15:40 07-11-4 Numerical Simulation of Direct Action Liquid Rocket Engines Hydromechanical Flow Conteollers Iana Bakhmet, Zhang Lihui Beijing University of Aeronautics and Astronautics, China Effect of angle between the primary and auxiliary holes of an anti-vortex film cooling hole Younggi Moon, Soon Sang Park, Jung Shin Park, Jae Su Kwak Korea Aerospace University, Korea Thermal-flow Characteristics of Double-Jet Film Cooling Holes with Various Transverse Trench Configurations Moon-Young Cho, Youn-Jea Kim Sungkyunkwan Univerisity, Korea. A Numerical Study of the Flow Dynamics of Through-type Pintle Nozzles with Large Scale Separation Flow Ki-Yeon Jeong, Jun-Young Heo,, Hong-Gye Sungb Korea Aerospace University, Korea (193) (313) (326) (354) 15:40-15:55 07-11-5 15:55-16:10 07-11-6 Experimental Study of Surge and Rotating Stall Occurring in High-speed Multistage Axial Compressor Changzheng LI, Siqi XU, Zhiqi HU Northwestern Polytechnical University, China Analysis of aerodynamic design characteristics of Flade fan ZENG Yueliu, WEI Yuan National Key Laboratory of Science and Technology on Aero-Engines Aerothermodynamics, Beihang University, China (405) (428) Session 8-10 Simulation of Hypersonic Cases 16:30-18:00 16:30-16:45 07-12-1 16:45-17:00 07-12-2 17:00-17:15 07-12-3 17:15-17:30 07-12-4 17:30-17:45 07-12-5 17:45-18:00 07-12-6 Aerodynamic Design and Numerical Simulation of Over-Under Turbine-Based Combined-Cycle (TBCC) Inlet Mode Transition Xiang Xianhong,Liu Yuan,Qian Zhansen AVIC Aerodynamics Research Institude, China Aviation Key Laboratory of Science and Technology on High Speed and High Reynolds Number Aerodynamic Force Research, China Real Gas Effect on a Standard Model Electre Junhong Li, Honglu Pan, Liang Zhang, Wenbo Miao, Zhi Chen, Xiaoli Cheng, China Academy of Aerospace Aerodynamics, China Numerical Study on the Stability of Hypersonic Wake Flow over Blunt body and Global Stability AnalysisDehua Zhu,, Qing Shena, Xiangjiang Yuan China Academy of Aerospace Aerodynamics, China Effect of recession on the re-entry capsule aerodynamic characteristic Xu Guowu, Zhou Weijiang, Chen Bingyan, Zhan Huiling, Yang Yunjun China Academy of Aerospace Aerodynamics, China Aerodynamic Design Optimization of a Kind of Reentry Capsule Based on CFD and Multi-objective Genetic Algorithm Wang Rong,, Chen Bing-yan, Zhang Hong-jun, Zhou Wei-jiang, Bai Peng, Yang Yun-jun The First Institute, China Academy of Aerospace Aerodynamics, China Detached Eddy Simulation on Hypersonic Base Flow Structure of Reentry-F Vehicle Chen Zhi, Zhang Liang, Li Pengfei China Academy of Aerospace Aerodynamics, China (160) (60) (22) (41) (65) (121) Session 8-11 Intelligent Computing, Communication and Control 18:10-18:55 18:10-18:25 07-13-1 18:25-18:40 07-13-2 18:40-18:55 07-13-3 Assessment Model of the Architecture of the Aerospace Embedded Computer Wei Han, Xiaoying Bai, Dep. of Computer Science & Technology, China Jianchun Xie AVIC Computing Technique Research Institute, China Covariance upper bound controllers considering intermittent packet losses of control and measurement signals Seungeun Kang, Sangho Ko Korea Aerospace University, Korea Key Techniques Research on UAV Data Link Jinxi Li, Yongfei Ding, Zheng Fang China National Aeronautical Radio Electronics Research Institute, China (98) (327) (462) APISAT-2014 2014 Asia-Pacific International Symposium on Aerospace Technology Online registration address: apsiat2014.csaa.org.cn. program Registration On-site registration location: Pullman Shanghai South Hotel Lobby Registration fee Member Non-Member Student Member None-member Student Early-bird registration (Before Aug. 25,2014) 2800RMB 3100RMB 1400RMB 1700RMB Late registration On-site registration (Aug. 26-Sep. 16) (Sep. 17-26) 3400RMB 4000RMB 3700RMB 4300RMB 1700RMB 2000RMB 2000RMB 2300RMB Notes: 1.Member refers to member of the following societies: Chinese Society of Aeronautics and Astronautics (CSAA) The Royal Aeronautical Society (RAeS) The Korean Society for Aeronautical and Space Sciences (KSAS) The Japan Society for Aeronautical and Space Sciences (JSASS) 2.Registration can only be processed after payment is done. Those who finish online registration before the early or late bird registration deadline but fail to pay can not enjoy the favored price. 3.Authors shall register and pay before the early-bird registration deadline. 4.For onsite registration, only RMB is accepted. 5.For technical visit, please register before the late registration deadline. Registration inclusions Ÿ Attendance at all scientific sessions Ÿ Morning and Afternoon coffee breaks Ÿ Materials: a symposium bag, proceedings on a CD-ROM or USB flash drive, final program including abstracts, name badge Ÿ Reception dinner on Sep. 24 (Except students) Ÿ Lunches on Sep.24 and Sep.25 Ÿ Banquet on Sep.25 (Except students) Ÿ Post tour on Sep.26 (Except students) Students and accompanying persons can buy extra tickets for reception, banquet and post tour at the following price: An extra reception dinner coupon is 300 RMB. An extra banquet coupon on Sep. 24 is 400 RMB. An extra post tour ticket is 500 RMB. Proceedings and Paper Publication Policy All accepted papers will be available on a CD-ROM for communication purpose. After the conference, the APISAT2014 proceedings will be officially published online by Elsevier (http://www.elsevier.com/) on its journal of Engineering Procedia. The online publishing takes 8-12 weeks. Once being published, it will be indexed by the database of Scopus and Science Direct instantly. It will also be evaluated for the inclusion of EI (the Engineering Index) and CPCI-S (Conference Proceedings Citation Index – Science, formerly known as ISTP). 37 APISAT-2014 2014 Asia-Pacific International Symposium on Aerospace Technology program The publication requires 1200 RMB for each paper within 5 pages, including figures and tables. Each extra page will require an additional 200 RMB. The payment must be made before Aug. 25, 2014. Upon publishing in October, the author will be asked to sign a copyright transfer declaration by Elsevier. Foreign authors are extremely welcome to publish papers on the APISAT2014 Proceedings to make it more international. The APISAT2010 Proceedings has already been indexed by CPCI-S. Oral Presentation Each orally presented paper is assigned 15 minutes, including Q & A. Authors please prepare Power Point for it. Present in the morning of Sep. 24, authors should upload their Power Point files onto the conference computer during the morning coffee break (10:45-11:00) . Present in the afternoon, authors shall upload their Power Point files onto the conference computer during 13:00-13:30. Detailed arrangement of parallel sessions can be found in this program. Methods of Payment On-line payment Online payment during online registration is strongly recommended. It’s convenient and quick. Bank Transfer Domestic authors can choose to pay through bank transfer. Please notify APISAT and your name in the remittance information column. The commission fee shall be borne by the remitter. Confirmation After payment is done, a confirmation letter will appear on the screen with the word of “confirmed”. It means you have finished online registration successfully. Otherwise, it means you have not finished online registration. Please print the confirmation letter and take it to the check-in desk. Cancellation of registration and refund Cancellation must be received in writing no later than Sep. 5, 2014. 15% of the registration fee will be charged as administration cost, the rest will be refunded; cancel after this date or fail to attend, no money will be returned. Invoice Chinese authors can gain their invoice for both the publication fee and registration fee upon check-in on Sep. 23, 2014. 38 APISAT-2014 2014 Asia-Pacific International Symposium on Aerospace Technology program Social Events Note: Full delegates(non-student) can enjoy social events for free. Students and accompanying persons to attend them shall buy coupons during online or on-site registration . The reception is 300 RMB per person, banquet 400 RMB per person and post tour 500 RMB per person. Welcome Reception Date: Wednesday, September 24, 2014/ 19:00 - 20:00 Venue: Ballroom 1+2, 3rd Floor, Pullman Shanghai South Dressing code: Smart Casual Banquet Date: Wednesday, September 25, 2014/ 19:00 - 20:30 Venue: Ballroom 1+2, 3rd Floor, Pullman Shanghai South Dressing code: Suit and tie Experience a truly special night in Shanghai, China at Banquet. Great food will be served accompanied by a colorful performance. We believe this event will provide you an unforgettable evening in Shanghai. This event is admissible by a ticket included in registration fee. Tickets are available for students and accompanying persons. Please the banquet in formal dress. Programme for Performance at Banquet for APISAT 2014 19:00 Commencement of performance 19:00-19:08 Opening performance: Face Changing in Sichuan Opera 19:08-19:10 Opening words of host (introduction to distinguished guests) 19:10-19:20 Peking Opera 19:20-19:28 Magic show (Latin dance & magic show) 19:28-19:30Toast 19:40 Banquet after performance Chinese Traditional and Modern Art Performance Date: Wednesday, September 25, 2014/ 19:00 - 19:30 Venue: Ballroom 1+2, 3rd Floor, Pullman Shanghai South The art performance will be held during the Banquet. The performance will provide 30 minutes wonderful and exciting Chinese traditional and modern show. 39 APISAT-2014 2014 Asia-Pacific International Symposium on Aerospace Technology program APISAT Post Tour A post tour program will be provided for all APISAT participants and persons with additional tickets. This event is composed of visiting the technical site as well as the well-known sightseeing place in Shanghai on September 26 (Friday). Please be advised that the post tour is offered free to only registered foreign participants. Students and accompanying persons who wish to join this event should pre-register at the website with the fee. Dressing Code: casual Date Sep. 26 Friday Time Function Location 9:00-11:30 Technical visit to COMAC Shanghai Aircraft Manufacturing Center (SAMC) Meet in front of the venue at 9:00. Depart at 9:10 on time. Coupon is required. 12:00-13:00 14:00-17:00 17:30-18:30 19:00-21:00 21:00 Lunch Visit Shanghai Museum Dinner Cruise on the Huangpu River Back to the hotel Shanghai Museum As a museum of ancient Chinese art, Shanghai Museum possesses a collection of over 1000,000 objects, about 120,000 of which are precious national-graded works of art. Its rich and highquality collection of ancient Chinese bronze, ceramics, painting and calligraphy is specially celebrated in the world. Founded and first open to the public in the building previously of the horseracing club at 325 W. Nanjing Road in 1952 and then moved into the former Zhonghui Building at 16 S. Henan Road in 1959, the museum developed very quickly in aspects of acquisition, conservation, research, exhibition, education and cultural exchanges with other institutes. In 1992, the Shanghai municipal government allocated to the Museum a piece of land at the very center of the city, the People's Square, as its new site. The whole construction took three years, from August 1993 to its inauguration on October 12th, 1996. The 29.5 meters high new building has a construction space of 39,200 square meters. Its unique architectural form of a round top with a square base, symbolizing the ancient Chinese philosophy that the square earth is under the round sky, is a distinguished architectural combination of traditional feature and modern spirit. The present Shanghai Museum has eleven galleries and three special temporary exhibition halls. It extends warm welcome to the visitors from all over the world. 40 APISAT-2014 2014 Asia-Pacific International Symposium on Aerospace Technology program Huangpu River Night Cruise The Huangpu River is the mother river of Shanghai. Nanpu Bridge, Yangpu Bridge and Oriental Pearl TV Tower compose of a huge picture scroll. The Bund is the cultural section of Shanghai that best represents the blending of ancient and modern influences. This renowned waterfront district is the city's most famous landmark. Local people honor the Huangpu River as Mother River, and as you view the lights and spectacle from the deck of your evening cruise, you will understand why. Between the stately colonial edifices along the Bund, the glittering skyscrapers on the eastern shore of Pudong, and the unceasing river traffic, there is plenty to keep your eyes from ever resting. Besides offering a privileged view of the bridges that span the Huangpu, the cruise boats also offer an excellent view of the famous colonial-era buildings that make up the Bund, buildings such as the Peace Hotel with its unique pyramid roof in blazing green and the Customs House with its large clock tower. The main ticket office of Huangpu River Cruise is opened daily, and the schedule usually includes a full morning cruise (from 9am to 12:30pm) and a full afternoon cruise (from 2 to 5:30pm). Both these full cruises make a complete circuit of the Huangpu to its mouth. The Huangpu River cruise company also offers a night cruise from 7 to 9pm, splendid when the lights are on the Bund and Pudong, but this voyage does not go downriver to the Yangtze. Cruise schedules vary depending on the season, and on weekends additional cruises are sometimes added. 41 APISAT-2014 2014 Asia-Pacific International Symposium on Aerospace Technology program General Information Conference Venue Pullman Shanghai South Hotel Location To Hongqiao Airport: 15 KM To Pudong Airport : 46 KM To Shanghai South Station: 0.8 KM To Caohejing High Tech Park: 3 KM To Shanghai Stadium : 3.5 KM To Xujiahui : 4.5 KM To The Bund: 12 KM Add: No. 1, Shanghai Pubei Rd. China, Post code: 200235 Tel: 021-24268888 Fax: 021-24268999 42 APISAT-2014 2014 Asia-Pacific International Symposium on Aerospace Technology program Transport information 1.Taxi It takes about half an hour for a taxi to arrive at the hotel from Shanghai Hongqiao International Airport and costs about RMB 50 (in daytime) or 70 (at night); while it takes about one hour for a taxi to arrive at the hotel from Shanghai Pudong International Airport and costs about RMB 160 (in daytime) or RMB 220 (at night). The above does not take any traffic jam into consideration. 2.Subway From Shanghai Pudong International Airport to Pullman Shanghai South Maglev train From Subway line 1 Subway line 2 Taking about 2 hour and 10 minutes Shanghai Pudong International Airport Taking Maglev train at the airport 1 station Getting off at Longyanglu Stop Take Subway line 2 (in the direction to Xujingdong) 7 stops Getting off at Renminguangchang Station Transferring to Subway line 1 (in the direction to Shenzhuang) 410 m Getting off at Shanghai South Walking to Pullman Shanghai South to 970m Pullman Shanghai South 43 APISAT-2014 2014 Asia-Pacific International Symposium on Aerospace Technology program From Shanghai Hongqiao International Airport to Pullman Shanghai South Subway Line 10 Subway Line 3 Taking about 1 hour and 10 minutes Shanghai Hongqiao International Airport From Walking to the subway station at Terminal 1 of the airport 820 m Taking Subway Line 10 (in the direction to New Jiangwan City) and getting off at the Hongqiao Road Station 6 stations Transferring to Subway Line 3 (in the direction to Shanghai South Railway Station) 260 m Taking Subway Line 3 (in the direction to Shanghai South Railway Station) and getting off at the Station for Shanghai South Railway Station (Exit 6) 5 stations Walking to Pullman Shanghai South 1.2 km Pullman Shanghai South to 3.Bus From Shanghai Hongqiao International Airport to Pullman Shanghai South Airport Bus Line 7 From Shanghai Hongqiao International Airport Walking to the airport bus station at the airport 30 m Taking Airport Bus Line 7 and getting off at the station for Shanghai South Railway Station Walking to Pullman Shanghai South to 44 Pullman Shanghai South 1.6 km 4 stations APISAT-2014 2014 Asia-Pacific International Symposium on Aerospace Technology program Accommdation We have negotiated favored price for APISAT2014 delegates at the conference venue and a few others with different levels around it. Pullman Shanghai South (Conference venue) Pullman Shanghai South is an international upscale business hotel, ideally situated in Star Plaza, which comprises of a commercial building and a four-storey shopping mall in the new CBD of south Shanghai. Room type Superior King Room Superior Twin Room Rate (per night) CNY880 CNY980 Incl. 1 breakfast buffet included 2 breakfast buffet included To reserve, please fill out the RESERVATION SHEET and return it to the hotel before Sep. 6, 2014. The sheet can be downloaded from: http://apisat2014.csaa.org.cn/pages/accommdation We strongly recommend you to reserve early. Other Options NO 1 Hotel & Star Room type Shanghai Everbright Standard room Int’l Hotel (Twin bed) ★★★★ Discount Rate (CNY) 480 2 H . Hotel ★★★★ Standard room (Twin bed) 450 3 JinJiang Inn(Long Cao Road) Standard room (Twin bed) 269 Conference venue 10mins to Pullman on foot/ 5mins by taxi Service fee/breakfast/ internet access included 15mins to Pullman on foot/ 8mins by taxi Service fee/breakfast/ internet access included Pullman on foot/ 10mins by taxi Service fee/breakfast/ internet access include To reserve, please fill out the reservation sheet and return it to Beijing Wanlixing Conference Service Co., Ltd. The form can be downloaded from http://apisat2014.csaa.org.cn/pages/accommdation Contact: Tom Zhu and Jerry E-mail: wlxli@vip.sina.com; Tel: 86-10-56385301/56385348 Fax: 86-10-56385348 Mobile: 86-13439260120/13381165301 45 APISAT-2014 2014 Asia-Pacific International Symposium on Aerospace Technology program Currency Local Currency Chinese currency is called Renminbi (literally people's currency), often abbreviated as RMB. Issued by the People's Bank of China, it is the sole legal tender for both the Chinese nationals and foreign tourists. The unit for Renminbi is Yuan, Jiao and fen. The conversion among the three is: 1 Yuan = 10 Jiao =100 Fen. Chinese people normally refer to Yuan as Kuai, Jiao as Mao. RMB is issued in both notes and coins. The denominations of paper notes include 100, 50, 20, 10, 5, 2 and 1 Yuan; 5, 2 and 1 Jiao; and 5, 2 and 1 Fen. The denominations of coins are 1 Yuan; 5, 2 and 1 Jiao; and 5, 2 and 1 Fen. Credit cards can be accepted at most hotels, tourist shops and some department stores. Currency Conversion One can change money upon arrival at the international airports of Shanghai. Also most hotels offer foreign exchange services and exchange cash and travelers cheques. The Bank of China exchanges money and travelers cheques. In China, wherever you exchange money the same day, the exchange rate is the same. Banking Hours: Mondays to Fridays, 9 a m to 5 pm. Foreign Exchange There are no quantitative restrictions imposed on foreign currencies, traveler's checks, or credit cards brought in. Inbound passengers carrying foreign currencies in cash of more than 5,000 U.S. dollars should declare to the Customs. The Customs shall release it on passengers' departure upon the declaration made at the last entry. Without last time declaration record of foreign currencies in cash, or if the recorded amount is less than what the passengers carry this time, the Customs shall release the discrepancies upon certificate issued by the Foreign Exchange Bureau or its authorized banks. RMB The limit of RMB allowed to bring in or take out of China is 20,000 yuan. Voltage Electricity is supplied at 220 volts, 50 cycles 46 APISAT-2014 2014 Asia-Pacific International Symposium on Aerospace Technology program About Shanghai Entering Shanghai, you will immediately be overwhelmed by the hustle and bustle of a thriving city: itscolours, its people, its futuristic skyscrapers and indigenous Shikumen houses. Check out this sectionbefore coming to Shanghai. Shanghai Location Shanghai literally means the city by the sea. Shanghai is situated at 31o14' north latitude and 121° 29'east longitude, on the west shore of the Pacific Ocean. It is bordered on the north and 47 APISAT-2014 2014 Asia-Pacific International Symposium on Aerospace Technology program west by Jiangsu Province , on the south by Zhejiang Province, and on the east by the East China Sea . Right in the middle of China's east coastline, Shanghai is an excellent sea and river port, boasting easy access to the vast hinterland. The city is divided into two parts by the Huangpu River: Puxi (west of the Huangpu River) and Pudong (east of the Huangpu River). Puxi is the older part of the city and hosts the majority of shops, restaurants and museums. Pudong is the modern part, and is recognized for its rather unusual yet extremely impressive high-rises such as Shanghai's tallest buildings, the Shanghai International Financial Center, Jinmao Building and the Oriental Pearl TV Tower. Shanghai Population Due to constant inflow of people from other parts of the country, the size of population in Shanghai keeps growing. Before Shanghai was liberated in 1949, it only had a population of 5.2 million.According to the Shanghai Statistics Bureau, Shanghai's population of residents with permanent residence registration had grown to 24.15 million, among which 14.25 million were long-term residents and 9.9 million were immigrants by the end of 2013. Shanghai Weather & Climate With a pleasant northern subtropical maritime monsoon climate, Shanghai enjoys four distinct seasons, generous sunshine and abundant rainfall. Its spring and autumn are relatively short compared with summer and winter. The average annual temperature is 18 degrees Celsius. The city has a frost-free period lasting up to 230 days a year. The average annual rainfall is 1,200 millimetres (about 50 inches). However, nearly 60% of the precipitation comes during the May-September flood season, which is divided into three rainy periods, the Spring Rains, the Plum Rains and the Autumn Rains. The highest temperature is in July and August. For ten days or so in these two months, the temperature can reach 35 degrees centigrade. The coldest period is from the end of January to early February - usually during the Chinese Spring Festival. This awfully cold period will last for about three days but it seldom snows. From March to May, the conditions are pleasant so this is the best season for traveling. The 'Plum Rain Season' is from mid-June to early July. From late August to the first twenty days of September, the city is also susceptible to typhoons, none of which in recent years has caused considerable damage. Generally you will need a light coat and sweater in spring and short- sleeved shirts in summer. In autumn, long-sleeved shirts, sweater and coat are necessary, while sweater and overcoat are appropriate in winter. 48 APISAT-2014 2014 Asia-Pacific International Symposium on Aerospace Technology program Weather averages for Shanghai Month Jan Feb Mar Apr May Jun Jul Aug Sep Oct Nov Dec Average high °C (°F) 8 (46) 8 (46) 13 (55) 19 (66) 25 (77) 28 (82) 32 (90) 32 (90) 28 (82) 23 (73) 17 (63) 17 (63) Average low °C (°F) 1 (34) 1 (34) 4 (39) 10 (50) 15 (59) 19 (66) 23 (73) 23 (73) 19 (66) 14 (57) 7 (45) 2 (36) Precip-itation mm (inches) 48 (1.89) 58 (2.28) 84 (3.31) 94 (3.7) 94 (3.7) 180 (7.09) 147 (5.79) 142 (5.59) 130 (5.12) 71 (2.8) 51 (2.01) 36 (1.42) Shanghai Tours & Sightseeing Highlights Shanghai has lots to offer for both first-timers and re-visitors. What are the Top 20 attractions in Shanghai? Shanghai has become a paradise for both shoppers and diners. Shanghai is studded with restaurants from time-honored eateries to a vast assortment of restaurants serving French, Italian and Japanese cuisine. Famous dishes from every major school of Chinese cooking are served at old villa restaurants. 49 APISAT-2014 2014 Asia-Pacific International Symposium on Aerospace Technology program The Bund - Shanghai Puxi Landmarks World Architecture at the Bund Add:Zhongshan Rd. (E1), Shanghai The Bund is a symbol of Shanghai. The Bund has dozens of historical buildings, lining the Huangpu River, that once housed numerous banks and trading houses from the United Kingdom, France, the United States, Italy, Russia, etc. The Bund houses 52 buildings of various architectural styles such as Romanesque, Gothic,Renaissance, Baroque, Neo-Classical,Beaux-Arts, and Art Deco. The buildings are harmonious in color and style, thus gaining the name of "Gallery of World Architecture". When night falls and the lights are on, all the buildings are lit with colorful lights, glistening and dazzling to the eye. Bund Sightseeing Tunnel Add: 300 Zhongshan Rd.(E1) (Puxi) 2789 Riverside Promenade(Pudong) Tel: +86 21 58886000 The 646.7-m long Sightseeing Tunnel at the Bund runs from the Bund at the end of Nanjing Rd. to the Oriental Pearl TV Tower in Pudong. It is the first of its kind for pedestrians in China . The tunnel adopts the internationally advanced SK system, taking 2.5-5-min.to cross the river. The interior wall of the tunnel is decorated with changing colors. The unmanned environmental, transparent carriages in the tunnel provide visitors with an open view. A 6-sound-band acoustic system accompanying the changing scenes, produces an effect on visitors of being present personally at the scene. 50 APISAT-2014 2014 Asia-Pacific International Symposium on Aerospace Technology program Waibaidu Bridge Add:East Daming Rd. cross Rd. of Huangpu Rd Spanning over Suzhou Creek, Waibaidu Bridge is a well-known bridge. It was first built in I 855 of wood and rebuilt in I 907 in iron and steel The bridge is 1 06.7-m long, with a load of 20 tons, a traffic lane of 11.2 m and 3.6-m wide sidewalks on both sides. It was once the most elegant and magnificent bridge in the city and, up to now, it is still considered one of the symbols of Shanghai. Huangpu River Cruise Add:153, 219-239 Zhongshan Rd.(E2) Tel:+86 21 63744461 The river cruise is an important traditional tourist item in Shanghai. The Huangpu River is the mother river of Shanghai. It symbolizes Shanghai and presents visitors with the cream of the city'S scenic sights on its banks. Here you will have a glimpse of Shanghai's past and look into the bright future of the city. Starting from the Bund the boat will bring you upstream to the Nanpu Bridge, turn around downstream to the Yangpu Bridge and all the way to Wusong Mouth, where the river meets theYangtzi, and then turns back. The cuise company owns different kinds of cruise ships, wharves and a waiting lounge. The company offers boat trips to Wusong Mouth to see the Three Layer-Water, Yangpu Bridge , Nanpu Bridge , the cuise of the “Twin Dragons Playing with the Pearl ”, boat charter service and special cuisse as required by tourists. Three on the Bund Add:3 Zhong Shan Road (E1), Shanghai Tel:+86 21 63233355 Web:www.threeonthebund.com Three on the Bund is a celebration of contemporary living where art, culture, food, fashion and wellness converge to inspire a richer life. The stunningly transformed neo-classical 1916 building is home to four unique restaurants, the Giorgio Armani flagship store, Space by Three private events space, Evian Spa by Three and the Shanghai Gallery of Art. 51 APISAT-2014 2014 Asia-Pacific International Symposium on Aerospace Technology program 52 APISAT-2014 2014 Asia-Pacific International Symposium on Aerospace Technology program 53 2014 Asia-Pacific International Symposium on Aerospace Technology preliminary Chinese Society of Aeronautics and Astronautics CSAA