Nondiffracting X Waves-Exact Solutions to Free
Transcription
Nondiffracting X Waves-Exact Solutions to Free
245 LEEE TRANSACPIONS ON ULTRASONICS. FwnOELECTRlCS, AND FREQUENCY MWIXOL, VOL 39. NO I , JANVAAY 1992 IY Nondiffracting X Waves-Exact Solutions to Free-Space Scalar Wave Equation and Their Finite Aperture Realizations Jian-yu Lu, Member, LEEE, and James F. Greenleaf, Fellow, E E E Abstract-Novel families of generalized nandiffracting waves have k e n discovered. The7 are exact n o n d i c t i n g solutions of the isotropic/homogenous scalar wave equation and are a generalization of some of the previoosly known nondiffracting waves the plane wave, Durnin,s beams, and the such to an infini@ portion of the M~~~ beam equation in of new beams. One subset of the new nondihcting waves have X-like shapes that are termed "X waves.'' These nondiffracting X waves can be almost exactly realized over a finite depth of field with finite apertures and by either broad band or bandlimited radiators. With a 25 mm diameter planar radiator, a zeroth-order broadband x wave will have about 2 5 mm lateral and 0.17 mm axial 6 d B beam widths with a -6-dB depth of field of aboot 171 mm. The phase of the X waves changes smoothly with time across the aperture of the radiator, therefore, X waves can be realized with physical devices. A zeroth-order hand-limited X wave was produced and measured in water by our 10 element, 50 mm diameter, 2.5 M H z PZT ceramicipolymer composite J o Bessel nondirfracting annular array transducer with -&dB lateral and axial beam widths of about 4.7 mm and 0.65 mm, respectively, over a -6-dB depth of field of about 358 mm. Possible applications of X waves in acoustic imaging and electromagnetic energy transmission are discussed. I. INTRODUCTION N 1983, J. N. Brittingham [I] discovered the first localized wave solution of the free-space scalar wave equahon and called it a self focus wave mode. In 1985, another localized wave solution was discovered by R. W. Zmlkowski [2] who developed a procedure to c o n m c t new solutions [3] through the Laplace transform. These localized solutions were Further studied by several investigators [4]-191. An acoustic device was conshucted to realize Z~olkowski'sModified Power Spectrum pulse that is one of the solutions of the wave equation through the Laplace transform [lo]. In 1987 J. Dumin discovered independently a new exact nondifkacting solution of the free-space scalar wave equation [XI]. Thissolution was expressed in continuous wave form and was realized by optical experiments [12]. Dumin's beams were further studied in optics in a number of papers [13]-1191. Hsu et al. [20] realized a Jo Bessel beam with a narrow band PZT ceramic ultrasonic transducer of nonumform poling. We made I Manurnipt iecelved April 10, 1991; revised and accepted June 17. 1991. by grant CA 43920 from the National This work was Npponed ih ~ ~ ~ t i tnF I ~ ~ . ..~ tH~~. .S~. The authors are wilh the Biadynamics Research Unit. Department of Physiology aad Biophysics, Mnyo Clinic and Foundation, Rochester: MN 55905 IEEE log Number 91203584. the h t Ju Bessel nondifFracting annular array transducer [21] withPZT ceramic/polymer composite and applied it to medical acoustic imaging and tissue [22]-[25], campbell era/. had a similar idea to use an annular array to realize a Jo Bessel nondiffracting beam and compared the JO Bessel beam to the Axicon 1261. [n this paper, we repon families of generalized nondiffracting solutions of the free-space scalar wave equation, and specifically, a subset of these nond~ffractingsolutions, which we term X waves (so-called X waves because of ole appearance of the field distribution in a plane throu)fh the axis of the beam). The X waves are a frequency weighted Laplace transform of the nondiffracliug portion of the Axicon beam equations 1271-[33] (in addition to the nondiffracting portion, the Axicon beam equation contains a factor that is proportional to fi that will go to infinity as z + XJ [31]) and travel in free-space (or isotropic/bomogeneous media) to infinite distance without spreading provided that they are produced by an in6nite aperture. Even a d h Enite apertures, X waves have a large depth of field. (For example, with 25 mm diameter radiator, a zerothorder broadband X wave will keep 2.5 mm and 0.17 mm -6-dB lateral and axial beam widths, respectively, and have a 171 mm depth of field that is about 68 times the -6-dB lateral beam width and 7 times the radiating diameter.) We have experhnentally produced a zeroth-order band-limited X wave [MI. We used our 10 element, 50 mm diameter, 2.5 MHz PZT ceramicipolymer composite JO -el nondiffracting annular array transducer [XI, [22]. The X wave had -&dB lateral and axial beam widths of about 4.7 mm and 0.65 mm,respectively, over a 6 - d B depth of hid of aboul358 mm. In comparison with Ziolkowski's localized wave mode [Z], [3], the peak pulse amplitude of the X wave is constant as it propagates to infinity because of its nondiffracling nature. Durnin's beams are nondiffracting at a single frequency but will diffract (or spread) in the temporal direction for multiple frequencies [22]. X waves are multiple freqwncy wares bur they nre nondiffracfing in both frajrrverse and ariol dzreclions. Like the Jo Bessel nondifEracling beam [21)-[25], X waves could be applied to acoustic imaging and tissue characterization. In addition, the soace and time localization vrooerties of . . x allow pafiicle-like energy transmission through large distances, as is the case with Ziolkowski's localized wave mode [7]. LO IEEE TRANSACnONS ON ULTRASOWCS. FERROELECIXICS. AND FREQUENCY CONTROL. VOL 39. NO. 1. JANUARY lq'X2 In Section 11, we first introduce the families of generalized nondiffracting waves and the nondiffracting X waves. Then, we prov~detwo specific X wave examples. The production of X waves with realizable finite apenure radiators and finite bandwidths are reported in Section IE.Finally, in Sections N and V, we discuss further impl~cationsof these novel beams. The exact solution of the free space scalar wave equation,@t, represents a family of nondifhacting waves because if one travels with the wave at the speed, c, i.e., z - rt =constant, both the lateral and axial complex field patterns, Ql(r, 4) and @z(z rt). will be the same for all time, t, and distance, a. I f r l ( k . C) in (6) is real, "=" in (5) will represent backward and forward propagating waves, respectively. (Ln the following analysis, we consider only the forward propagating waves. All 11. THEORYOF X WAVES AND TWO EXAMPLES results will he the same for the backward propagating waves.) We will show hclow three families of generalized nondiffracting solutions of the free space (or isotropic/bomogeneous) Furthermore, QC(s) and ari(s) will also represent families of nondiffracting waves if rl(k.C) is independent of k and C, scalar wave equation. The free space scalar wave equation in cylindrical coordl- respectively. These waves will travel to infinity at the speed of cl without diffracting or spreading in either the lateral or axial rates is given by directions. This is different from Brittingbam's focus wave mode [I], and Ziolkowski's localized wave [2] and modified "-0. (1) power spectrum pulse [3] that contain both z - d and z - d t , I F l ~ = I or both z - ct and z + c+ terns in their variables, where c and where = represents radial coordinate, d, is , are different azimuthal angle, z is axial axis. whtch is perpendicular to the we find mC(s) is 'he most interesting solution. In the plane defined by r and d,, f is timime and represents acoustic following, we will discuss @<(s) only. QC(s) is a generalized pressure or Hertz potential that is a function of r, (1, 2, and t. function that contains fiome of the nondiffracting solutions of The three functions below are families of exact solutions of the free space scalar wave equation known previously, such (1) (see the Appendix): as, the plane wave. Durnin's nondlffracting beams, and the nondiffracting portion of the Axicon beam in addition to an (2) infinity of new beams. $(s) = [T(k) J4v)f(s)&] dk If T(k) = li(k - k'), where S(k - k') is the Diiac-Delta -C function and k' =w/e > 0 is a constant, f ( s ) = e', rro(k,C) vr = -r@. b(k. C) = = iw/cl, from (2) and (5), one obtains (3) Du'"in9s ~ o ~ d i f h c t i n gbeam ,111 a )= - [ ( ) + + - n . [$ j )[ / -li -77 I QL(T,$. z - r t ) = @1(r.$)@?(z - cY) [Li QD(s) = - -= (4) where A(@)p-%"'CO'(6-fl)n() I p'(fl*-l) (8) where s = ( Y ~ ( ~ . < ) T(4 ~o s8) + b(k, <)[a & cl(k. C)t] /j= (5) ,,&GF (9) where n is a constant and w is angular frequency. If A(@)= i"+"', we obtain the nth-order nondiffracting Bessel beams: and where cl(k.C) = cJl+ [na(k, <)/b(k.~)]' (6) where T ( k ) is any complex function (well behaved) of k and could include the temporal frequency transfer function of a radiator system, A(@)is any complex function (well behaved) of 0 and represents a weighting function of the integration with respect to 8, f (s) is any complex lunction (well behaved) of s, D(C) is any complex function (well behaved) of C and represents a weighting function of the integration with respect to 5, which could be the Axicon angle ((I I)), rxo(k,t) is any oomplex function of k and (. b(k.0 is any complex function of k and 5. The term c: is wndant in (I), k and C are variables that are independent of the spatial position, r'= (rcos$, rsin$, a), and time, t, and Qz(a - ct) is any complex function of z rt. Ql(r,$) is any solution of the following transverse Laplace equation (an example of Ql(r, dl) is given in the Appendix): - [:$(';) 1 8' +;iw]@l(r,,i=~. Q Q 7, (.F) = J,, ( ( ~ T ) P ' ( ' ~ - ~ ~ + (n ~ ~= ) .0. 1. 2, . . .). (10) If n = 0, one obtains the Jo Bessel nondiffracting beam. From (S), it is seen that cl(kl, C) of the Dumin beams is equal to w//i and is dependent upon k'. Therefore, if T(k) in (2) is a complex function containing multiple kequeucies, a<(.?) will represent a dispersive wave and will dBract in the axial direction, a. If both 7~ and n are zero, (10) represents the plane wave [ll]. If in (2), we let T(k) = 6(k - k'). ,f(s) = e', A(@)= i"ee, cun(k,i)=-iksinc, b(k,C)= zkcosC, where k' =w/c > 0 is a free parameter, and C represents the Axicon angle (we confine 0 < C < ~ 1 2we ) ~obtain the nth-order nondiffracting portion of the Axicon beam [31]: (PAn(s) = ~ , ( k ' r sin ~ ) e ' ( " ' " ~ " ~ - " ' ~ + " * ) , (n= 0, 1, 2, ...). (11) From (1 l),it is seen that c1(k1,C) = clcosC is independent of k', which means that the waves constructed horn QA,,(B) by (2) LU ANU GREEM.EAF: NONDIPFRACITNG X WAVES will have a constant speed ci for all frequency components and will be nondispersive. The X waves derived in the following are such waves that are nondiffracting or nonspreading in both lateral and axial directions. We obtain the new X wave if in (2), we let T(k)= B ( k ) r - ' ~ ~ ,A(@)= znean8, ao(k,() = -iksinC, b(k,C) = ika)s<, f (s) = ee, obtaining zeroth-order nondfiacting X wave: a0 @SBB~ = + [a0 - i(zcosC - rt)12 2/(T sin (17) The behavior of the analytic envelope of the real part of (17). R e [ a . s ~ ~ is , ] shown in the upper left panel of Fig. 1 or Fig. 2. The modulus of @XBB" in (17) can be obtained as shown in (18) (see bottom of page). Now we discuss the lateral, axial, and X branch behaviors of this X wave. It is seen from (18) that for 6xed C and no, at the plane z = dlcosC we have This is an integration of the nth-order nondiffracting portion ((11)) of the Axicon beam equation multiplied by B(k)e-nok, where B(k) is any complex function (well behaved) of k and represents a transfer function of a practical radiator system, k =wlc, a0 > 0 is a constant, and is the Axicon angle [31]. From the previous discussion, it is seen that ex, is an exact nondfiacting solution of the freespace scalar-wave equation (1). Equation (12) shows that as,, is represented by a Laplace transform of the function, B(k)J,(krsinC), and an azimuthal phase term, ein*. Because the waves represented hy @x,have an X-like shape in a plane through the axial axis of the waves, we call them nth-order X waves. We finish this section with two new nondiffracting X wave examples. The first represents an X wave with broad bandwidth, white the second LF a band-limited X wave. Example I: First, we describe an expression for an X wave produced by infinite aperture and broad bandwidth. Lf, in (12), B(1r) -- ao, we obtain from the Laplace transform tables [35] < which represents the lateral pressure distribution of the X wave through the pulse center and has an asymptotic hehavlor proportional to l/r when r is very large. On the line r = 0, from (18), we obtain which is the pressure distribution of the X wave along the axial axis, a, and has an asymptotic behavior proportional to 1/ I z &t I when I z - +t I is very large. The pressure distribution of the X wave along its two branches (see Figs. 1 and 2) can be obtained when - sin C cos C where cos C c - IQo z - - t I > l ca? < and from (18) we obtain giving an nth-order broadband X wave solution (exact solution of (1). see the Appendix): @xsn, = a o ( r sin <)"em@ m(7+ mln \ , (n = 0, 1, 2, ...) (14) / where the subscript BE means "broadband," and M = ( r s i n ~ ) '+ 7' (15) and where r = [ao- i(z cos < - ct)]. (16) For simplicity, we let n = 0, obtaining axially symmetric which has an asymptotic behavior that is proportional to 114when z - +t I isvery large. This is the direction of slowest descent of the X wave ampl~tudefrom its center. From (19). (ZO), and (Z),it is seen that the smaller a,, is, the faster the function I @.yns, I diminishes as r or I z -t I increases. If sin< is small, the diminution of I (P.~:) will he slow with respect t o r and fast with respect ( . This means that if the X waves are applied to to I e- &f. I - IEEE lXA?\SACTlONS O h ULTi7ASONICS ~RROLLECIRICF.N FREQUENCY CONTROI.. VOL 39. NO. I. JANUARY 19% snndillincliily X u.llvc solution of Ihc free-spilcc rcnlal. wave cqualion. Panels (h), Fig. I. Pmel (a) ruprcsenls !he carul ren,li~-~rdci (c), and (d) are lhc ilppnlpriale rcmlh-order nundilfracling X waver cal~uiutedfrom !he Raylcigh-SnmmerfcId dilfraclion inlegral wiih a 25-rnm diamelsi planar radValilr a1 dirwncra :=YI mm. 9Ll mm. and !SO mm, re.ipeclively. The dirncnsion of each panel is 12.5 mm x 6.25 mm. U ( f i )= <!u. <= 4" bmd rr,, = 11.05 nmm. Fig. 2. Same fumlal :LS Fiz. 1. crcrpl ihiil r imaging, smaller ncj will give better resolutions in both lateral and axial directions, while smaller sin ( will reduce the Lateral resolution while increasing the axial resolution. At thecenter of the zeroth-order X wave ( r = 0. r = rf/cos C), Q s a s , 1 for all distance, z , and time, t (see (17)). which is unlike Z~olkowski'slocalized wave [2] and moditied power s p c m m pulses (11 that recover their pulse peak values periodically or aperiodically with distance, z. E.x~mple2:Because B(k1 in (12) is free. it may be chosen to achieve realizable bandwidth as shown in the following -- 50 rnm diamcmt piansr radiator is used example. If B ( k ) is a Blackman window function [36]: B ( k )= { R" b.32 - 0.Srori 0, 2 + 0.OXrori v]. 0 5 12 < 2L" otherwise (24) can approximate the bandwidt~,of a real transducer. Although we cannot find an analytic expression for Q.s., from using (24) in (12) by directly looking up a Laplace transform [able, we will describe in thesection El the resulting nondiffracting beam calculated for some 6nite apertures. we LU AND GREENLEAF: NONUFIRACTING X WAVES 3 111. REALIZATION OF 14 WAVFSWITI~ RNTE APERTURE RADLATORS The extension and therefore the apenure requirement of X waves in space is infinite (see (12)). But we show that nearly exact X waves can be realized with b i t e aperture radiators over large axial distance. To calculate X waves kom the b i t e aperture radiators. a specmm of X waves is used. Equalion (12) can be rewritten as (25) (see bottom of page). which is an inverse Fourier transform of the function (spectrum of X waves) ):( '"JB and F-' represents the inverse Fourier transform. The first and second terms in (30) represent the contribution from high and low frequency Because B ( w / r ) in @8) $ independent of r' and #. (30) can be rewritten in another form ( k )= B ( C) J , (>sin (I is the Heaviside step function P7J. At the plane z = 0. (26) becomes Lu' =B (11 = 0.1.2.. . .) (28) where The spectrum m (28) is used to cal~vlateX waves Gom radiators with finite aperture. If we assume that the radiator is circular and has a diameter of D,rhe Raylcigh-Sommerfcld formlilation of diffraction by a plane screen [38] can he written as and I):<( mB, (F. t )= F-I pa, , ) (32) +'2rr "(11 D(2 2~ kITz piiir.ol, r ' ~ l r ' ~ ~ . ( l4'' ..alix ,id1 "01 i) I) = 0 . 1. 2. ...) (33) I); ( )I an,,(7.t) = F-' [B (;)c,,(.?. (%) En,( r . z) , r c ~[j. . 0 (rl ), =0 1 2 pik.r.c~l where $. ($7 dl'. (26) (T, ) where . ( r e = 0.1.2.. . .) I".+, ) ( , = 0. 1. 2, ...) (31) where A is wavelength, roi is the distance between the observation point, F, and a point on the source plane (r'.4'). = F B ( 1* [ (34) where * denotes convolution on time, 1, and F '[B(w/r.)] can be taken as an impulse response of the radiator. We now deqcrihe an example of an X wave produced hy a finite aperture. Let B ( k ) = fro, C = 8". (sin4' r= 0.0598, cos4" r= 0.9981, nu = 0 05 nim, n = 0, and c = 1.5 mmib~r (speed of sound in water). The analytic envelope of the real R I ' [ @ Rcalculated ~]. fronl (33) and (34) is given part of an,,, in Fig. I and Fig. 2, when the d~ameterof the radiator, D, 15 25 mrn and 50 mm, respectively. The X waves are shown at ,- = 30mm, 90 mm. and 150 mm, respectively. These X waves compared well to the analytic envelope of the real part of where the exact nondiffracting X wave solution, RP[@.YBB,,], @yos,,is given by (17) (see upper-left panel of Fig. 1 or 2). Fig. 3 shows beam plots of thc X waves in Figs. 1 and 2. Figs. 3(al), 3(a2), and 3(a3) represent the lateral beam plots of the X waves produced at Lhe axial distances z =30 mm, 90 mm, and 150 mm, req)ectively, through the center of the pulses. The full, dotted, and dashed lines represent the beam plots of the X waves produced by a 25 mm diameter radiator, 50 mm diameter radiator, and the exact nondiffracting X wave solution of the free-space scalar wave equation (real pan of (17)), respectively. Fig. 3(a4) represents the peak of the X waves along the axial distance, z, from 6 mm to 400 mm. The 4 - d B depths of field of the X waves are about 171 mm and 348 mm when thc radiator has diameters of 25 mm and 50 mm, respectively. The -6dB lateral heam width throughout the depth of field i6 about 2.5 mm. I 24 TRANSACIIONS ON ULTRASONICS. FERROELELTRICS, AND R(EOUENCY CONTROL VOL 39 0'1 U'O 90 PO 20 00 epmlufiew p z p u u o ~ 0-1 8'0 SO C'o BPnllUSew psz,puuoN 1'0 0'0 LU AND G B E e N W . NONDlFFRACnNG X WAVES Fig. 4. RayleigMommerieid aiculalion 01' [he zemlh-ndcr nundill'rilcling X w;tves pmduucd hy a 25 nuu diameter. hand-limiled planar radiator at distances ;=30 mm. 90 mm, and 150 mm. Thc ritdi;dor lrilnslcr rundiun Lllkl is a Blackman window Function peaked at 3.5 MHz with a --(,-dB hilndwidlh about 2.88 MHz. The dirncnsian ol silch psnrl is 12.5 mm x 6.25 mm. C = 4' and a" =0.05 mm. Figs. 3(bl) to 3(b3) are axial beam plots of the X waves with respect to c l t - z and correspond to Fgs. 3(al) to 3(a3), respectively. ( e l = c/cos<. For ( = 4",cl ;= 1.002c.) The edge waves produced by the sharp mtncation of the pressure at the edge of the radiator are clearly seen. These edge waves can be overcome by using proper aperture apodizalion techniques [39] and will be discussed in the next section. The -6-dB axial beam width obtained from Fig. 3@) is about 0.17 mm. The depth of field and the lateral and axial beam widths of the zeroth-order broadband X wave produced by a radiator of diameter D can be determined analytically in the following. For any given angular frequency, wo,(30) represents a continuous field of an aperture shaded by a .lo Bessel function which is independent of frequency * a ! If C= -1" and D = 25mm, we obtain, from (39). z,,=178.8 mm, which is very close to what we obtained from Fig. 3(a)(4) (171 mm). The 6 - d B lateral beam w~dthof the X waves can be calculated from (19). whlch is and the -&dB axid beam width is obtained from (20) I. < 2 1 ; - t1-03 (=-. 2dnn cos < When no = 0.05 mm and i = 4*, the calculated -6-dB lateral and axial beam widths are about 2.5 mm and 0.17 mm, respectively, which are the same as we measured from Fig. 3. Figs. 4 and 5 are the analytic envelope of a zeroth-order hand-limited nondiffracting X wave produced by a radiatar of diameter of 25 mm and 50 mm, respectively, when B(L) is chosen as a Blackman w~ndowfuncuon (see (24)). The parameter ice in (24) for these figures is given by where and The depth of field of this JO Bessel beam is determined by L111 Substituting (37) into (38). we obtain Z, D = - rot 5 2 (39) where r. =1.5 mrnll~b,fo =3.5 MHz. and the -6-dB bandwidth of ihe Blackman window function is about 2.88 MHz. The X waves in Figs. 4 and 5 are a band-limited version of those in Figs. 1and 2. They are the finite aperture realization of the convolution of function F-l[B~~ic)]/nlr with (14) when ri = 0, that is IEEE TRANSACTIONS ON ULTRASONICS. FERROELECIWCS. ANII FREQUENCY CONTROL VOL 39. NO. I. JANUARY 1992 Fig. 5. Samr formal as Fig. 4. cxcepl lhal a 511 m m d i m e l e r planar radiator ir used. with n = 0, where B(lo/c) (w 2 Oj can be any complex function that makes the integral in (25) converge, "*" denotes the convolution with respect to time, t, and the subscript BL represents "band-limited." The three panels in Figs. 4 and 5 represent band-limited X waves at dislance z =30 mm, 90 rum, and 150 mm, respectively. The parameters <and ao are the same as those in Figs. 1 and 2, which are 4' and 0.05 mm, respectively. From Figs. 4 and 5 , it is seen that the band-limited X waves have lower field amplitude in the X branches than the widehand X waves in Figs. 1 and 2. Fig. 6 is the same as Fig. 3, except that it represents the lateral and axial beam plots of the band-limited X waves in Figs. 4 and 5. The 6 - d B lateral and axial beam widths of the band-limited X waves obtained from Fig. 6 are about 3.2 mm and 0.5 mm, respectively, at aU three distances ( z =30 mm, 90 mm, and 150 mm). Therefore, these band-limited X waves are also nondifhacting waves. Theu -6-dB maximum nondiffracting distances derived from Fig. 6 are 173 mm aod 351 mm, when the diameters of the radiators are 25 mm and 50 mm, respectively. The depths of field of the band-limited X waves are almost the same as those of the broad band nondiffracting X waves obtamed lrom Fig. 3 and are very close to those calculated from (39). Rayleigh-Sommerfeld formulation of diffraction 138) can be used to simulate the resulting beams. Besides the X waves. there are many other families of nondiffracting waves that are also exact solutions of the freespace scalar wave equation (see (3) and (4) and the Appendix). B. Resnluhon, Depth . of . Field, and Sidelobes o f X Waves From (IS), it is seen that as n, decreases, the X waves diminiqh faster with both r and I r - (el eos Ct) I, and hence they have higher lateral and axial resolution. This requires ihat the radiator system has a broader bandwidth because the lerm expi-aowjc) in (26) will diminish slower for smaller 0,). For larger values of sin 5, the lateral resolution will he increased while the axial resolution is decreased. The -6-dB lateral and axial beam widths of the zeroth-order broadband nondiffrscung X waves ((17))are determined by (40) and (41), respectively. For finite aperture, the X waves are nondiffracting only within the depth of fieId The depth of field of finite aperture nondiffracting X waves is related only to the s u e of the radlator and the Axicon angle C ((39)). Bigger values of sinC will increase the lateral resolution ((40)) but reduce the depth of field. This trade-off is similar to that of conventional focused beams. For band-limited nondiffracting X waves, the laleral and axial beam widths are increased from those of the broadband X waves, but the depth of field is about the same. JV. DISCUSSION The X waves have no or lower sidelobes in the (i - elt) plane than the .& Bessel nondtacting beam [21], see Figs. A. Other Nondiffmding Solutions 3 and 6. They do have energy along the branches of the X From (43). it is seen that an infinity of nondiffracting X that becomes smaller as the tadius r increases (see Figs. 1, wave solutions with lower field amplitude in their X branches 2, 4, and 5). It is fortuitous that the realizable band-limited X can be obtained by choosing different complex functions R ( k ) . waves piresent lower field amplitude in their X hmches than In practice, B ( k ) can be a h-ansfer function of physical de- the broadband X waves (Figs. 4 and 5). In acoustical imaging, vices, such as acoustical transducers, electromagnetic antennas the effect of energy in the X branches could be suppressed or other wave sources and their associated electronics. The dramatically by combining X wave transmit with dynamic - 28 I E E TRANSACCIONS ON ULTRASONICS. F ~OELFCTRICS,AND FREQUENCY CONTROL. VOL 39. NO 1. JANUARY 1992 spherical focused receiving as was proposcd fa1 the J" Bessel nondiffracting beam [2.5]. C. Edge Waves and Propagation Speed ofthe X Waves From (17).it is seen that at a given distance z, the X waves extend from t> - co t o t < m. Therefore, they are not causal. but the X waves produced by fininte aperture diminish very last as I t I -%. lf we ignore the X waves for I t I > t o , where I e.~,, (r'.to)I<< 1, these modified X waves can be treated as causal waves. Similarly. Ziolkowski's localized wave 121, and modified power spectrum wave 131 suffer from the problem of causality, but they are closely approximated with finite aperture by using this same causal approximation [10]. We do not wony about the superluminal solutions, noncausal solutions. infinite total energy or infinite apertures as long as the pressure distributions over an aperture are slrFficienLly well behaved that they can be physically realized and truncated in time and space and still produce a wave of practical usefulness. Theoreucal X waves are superluminal, ooncausal, and have infinite total energy and apertures, but rhey can be truncated to produce practical waves. One example waq given in reference [34], where a zeroth-order X wave was physically realized over a deep depth of field in an experiment using an acoustic annular array transducer [21], [22]. It is seen from Figs. 3@) and 6(b) that there is some energy in the waves produced by the edge of the aperture because of sharp truncation of the pressure at the edge of the radiators. These edge waves can be reduced by apodization techniques [39] that use window functions to apodize the edge of the aperture. (The results in Figs. 1 to 6 are obtained with a rectangular window aperture weighting.) Fig. 7 shows reduction of the edge waves with aperture apodization. Figs. 7(a) (except panel (4)) and 7(b) show the lateral and axial beam plots, respectively, of band-limited X waves produced by a 25-mm-diameter radiator. The full and dotted lines represent the beam plots before and after the aperture apodization, respechvely. The apodkation function is given by (44) (see bottom of page). where v1 = 3D/8, D is the diameter of the radiator, and r is the lateral distance from the center of Ule radiator. Panels (I), (2), and (3) in both Figs. 7(a) and 7(b) represent the beam plots at distance 2 =30 mm, 90 mm, and 150 rnm, respectively. Fig. 7(a4) plots the peak E. Application of X Waves to Acoustic Imaging value of the X wave along the axial axis from z =6 mm to and EIecrromagtie~icEnergy Tra~ismi.~sion 400 mm. The edge waves are reduced around 10 dB within The real part of (17), R C [ ~ ~ ~has ~ ,a ]smooth . phase the depth of field by the aperture apodization. Thc depth of t, across the transverse direction, r . This change aver time, field of the X wave is reduced from 173 mm to about 147 mm after the aperture apodization because of the reduced effective makes it possible to realize X waves with physical devices. Therefore, a broadband acoustic transducer could be used size of the aperture. to produce X waves in Figs. 1 to 3, while a band-limited From f17). it is seen that the X waves travel with a speed transducc~ could generate those in Figs. 4 to 6. The electrodes faster than sound or light speed, c (superluminal). For example, of an acoustic broadband PZT ceramictpolymer composite If C = J", the X waves will travel about 0.2% faster lhan r. transducer can be cut into annular elements [21] and each This is also the case of Durnin's Jo Bessel beam. From (10). elcmcnt driven with a proper waveform depending upon its for 71 = (1, we obtain radial position. Annular array transducers can be used for both X wave transmitling and conventional dynamically spherical focused receiving [34]. The low sidelobes of a Gaussian < k. Theretore. c =w/k < shaded receiving would suppress the off-center X wave energy where cl = w//3 and ll = PI. and produce high resolution, high frame rale, and large depth This is explained in the following: For large radius, r, on of field acoustic images. the surface of a radiator, the wavefront of the X wave is The X wave solution to the free-space scalar wave equation advanced. It is these wave fronts that construct the X wave csn also be applied lo electromagnetic energy transmission for at large distances as the lneuence of the wave fronts from the private communication and military applications [q.(Noncenter of the radiator dies out. The wave energy radiated from diffracting electromagnetic X waves are discussed in detail in each side of the radiator travels at the speed of sound. r.. but r401.1 the intersection, or peak. of these waves travels greater than the speed of sound. D. Total Energy, Energy Dettsir?.U J I ~Causality Like the plane wave and Durnin's beam, the total energy of an X wave is infinite. But, the energy densi~yof all these waves is finite. Approximate X waves are realizable with finite apertures and with finite energy over a deep depth of field. We have developed a new family of nondiffracting waves that provides a novel way to produce focused beams without lenses. They are realizable with finite apertures and with broadband and band-limited planar radiators w ~ t hdeep depth of field. The energy on the X branches of the X waves could be suppressed dramatically in maging by combining the X LU AND GREENLMF. NONDIFFRACrING X WAVES I -- 3II UCB TRANSACIIONS ON ULTRASOMCS. FWIROELECTRLCS. AND FREQuoVCi waves with a conventional dynamically spherical focused receiving system to produce high contrast images 1221. Characterizahon of tissue properties could be simplified because of the absence of diffraction in X waves. In addition, the space and time localization properties of X waves will allow particleltke energy transmission through large distances, as is the case of Ziolkowski's localized wave mode [7]. APPENDIX CDWROL VOL 39. NO I. JANUARY 1992 Now we prove e L ( s ) in (4) is also an exact solution of (1): Because @l(r,d) is an exact solution of the transverse Laplam equation ((7)). the right-hand side of (54) is zero. ThLs proves that @L is an exact solution of the free-space scalar wave equation (I). For example, if we choose Q ~ ( z ct) as a Gaussian pulse Theorem: Functions @f(s), P,K(.v), and mL(s) are exact solutions of the free-space scalar-wave equatton (1). are linear sumProofl The functions QC(s) and *2(t - d )= e-(:-ct12/"l mations of function f (B) over free parameters k and C, respectively, see (2) and (3). Therefore, if we can prove f (s) and Ql(r.4) as Poisson's formula 141, p. 3731 is an exacl solution of (I), @C(s) and ah-(s) will also be exact solutions. 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Park, "Analysis of bmadband ulhasoniu field rcsponse and ils application to lhc design of focused annulsr mu?. imaging syslcmr.' Ullraron. Tcchnol. 1987, Toyohachi IB. Cod. Ullraron. 'Technol, Toyohashi, Japan. Edilcd by Kohji Toda, MYU Res.. Tokyo. 19H7. 14111 J. Lu and J. F. G~cenleaf,"Nondiflracting eleclromrgneiic X waves: IEEE Tro,t.t Anrpnnos Propng.. submilled for revirw. 1411 P. M. Make and H. Feshbaeh. MeiE~odrof T7reorerico1 Pl~ysies,Part I. NEWYurk McGmw-Hill. 1953. chs. 4 and 7. Jian-yu Lu (M'88) was ham in Fwhou. Fujian Province. Pcople's Republic of Chins. an A u g s t 20. 1959. He received the B.S. degree in elcclrical engineering in lY8Z Erom Fudan University. Shanghni, Chin*, Lhe M.S. degree in Ill85 fmm Tnngji University, Shanghai. China, and the Ph.D. degree in 1988 frnm Sootheast Univenily. Nanjing, China. He is an Assistant Prnfessnr olBiophgsicr. Maye Mcdical School. and a Research Assnciule. at the Biodynamics Rcsearch Unil. Dcpanment ofPhysiology and Biophy~ic.;.Mayo Clinic and Foundalion. Rnchesler, MN. Prom 1988 lo lYq(1. he was a postdnctoral Research FeUow Ihcre. Prior to that, he was a kcacully mcmher of the Dcp;lrlrnenl of Biomedical Engineering, Sdulhcasl Univmily, :nrd worked with Prof. Xu Wei. His research interesls are in acoustical imaging and librue characlerhttion, medical ullrasanic Iransdurrrs. itnd nondifliubing wiwc transmission. Dr La is u member of the I E E UFFC Society. the American institute of Ultrasuund in Medicine. and Sigma Xi. James F. GreenleaF(M'7.?-SM'8GF'88)was horn in Salt Lake Ciy. UT. on Fcbnrilr/ 10, 1942. HI. received the B.S. degee in electrical engineering in 1964 born the University o f Utah. Salt Lake City. the M.S. degrcc in engineering science in 1968 from PurdueUnivcnity, Lafayette, IN. and the Ph.D. degrce in engineering science from Lhe Mayo GTrduate School or Medicine. Rwhesrer. MN, and Purduc University in 197f1. He is a Professor o i Biophysics and Medicine, Mavo Medical School. and Consultant. Biodvnamics Rcscuch Unit. Depnrtrnenl of Physiology, Biophysics, and Cnrdiavuscuiar Dise.~xe and Medicine. Mayo Foundation. Dr. Greenled- has served on Lhe IEETechnical Commiltcc of thc Ultras o n i s Sympusium since 1%. He served on Lhe IEEE-UFFC Suhcommiltou lor the Ultrasonics in Medicine/lE!Z Measurement G~lidcEdiloa, and on lhe IEEE Mcdiusi Ultrasound Committee. He is Vice Preridcnl of the UFFC Sociay, Hc holds Ave patents and is the recipienl of the 1986 1. Holmes Pioneer award form the American rnstirutt of Ultrasound in Medicine, and is u Fellow of the IEEE and ihc ANM. He is thc Distinguished Lecturer for the E E W C Society for 1991!-1991. 13s spacial lield of iaerest is in ullraonic hic~medicalimaging science and hss published more than 150 articlcs and edited four hooks.