1178 taken london rotation accurately shown 1630 nml electronic bay na 495 latl arc frequen mild interesting ron conducting excitation appropriate experimentally fte JL show skew 6•35 better 272 panel spend already knowledge inserted 0408 resonant unstiffened square latter approximately the• position table whenever exposure delay 1510 wa set real theoreuad deviation missile MH missed OLSON research considering 2281 ata both 1146 395 located peak would nodal object existence interferometry fimire third PAVITHRAN hub deviate duignun developer clamped academic bottom STIFFENED grateful closely 30C rigidly higher inn mental globally 2180 save dynamic appear rectangular usual 1545 area hnc stiffnes exist INTRODUCTION right necessary 165 natural extent investigated meat 2428 represented idealisation simple desired oilier 149 aircraft commonly expected BS tuned rib pre intensitie causing compatible brightly bangalore many intensive finite numerical 1257 author L2 provide 382 canti I5I5HZ dark remaining understanding 940 presented 1056 account combination away DISCUSSION H50 cmployed seldom increase sec untinodal canada published later 1245 turn iron 1763 introduced under MI frequencie sequence our earlier determined zone velocity i'varying of'aircraft angle 1272 STUDIES permit 310 theory sti without than just interfcrometric 850 1360 reduction follow 2000 concentration image RIB 30o order following data uu vibration after back 855 india uncut ilu departure difference matrice wave magnetic 1799 conslant rapidity respectively needed dwfiy cusch mule actual 45o holder generated structurally moat theo RESULTS physic 5BQ compared characteristic mojc 3it extensive averaged method any 905hz more material regarding eliminating report most PLATES msulc triangular riww parative sca again aeronautic flexibilitie phase much procedure part cqut left experiment fact ol'associated seen upon only sweep absolutely recorded structural reasonable producing OF approache represen into good phtiikmwation thicknes state wer 0022 flat associated 2528 1026 depending percentage 400 pen introduction 1977 mis fixed thcore paper received 02' hi next almost value displacement cast science anti august input 806 some function quadrature 1605 REFERENCES financial respect durvasula location society IM missing aspect 7H3 IVU tto RFI employed vector helween aero cathode variation 1H05 accurate K'0 com display lindbi'iui 465 pewenttw oscilloscope 385 PROCEDURE bending 847 studying consider behaviour variou design studie teristic frequence 2255 other term investigator except retically principle ponding view 114x 397 ann stres 401 nuixunum dispiacement well sharp DURVASULA pres followed beam mall indicating directed cie form give precision figure node being scanned may 783 different reconstructed mid llw 1025 regard plelcly width 0389il02 comparative 897 237 test 2722 their retained scale best therefore included far carried appcan required also sound distribution but over schematic 983 agreement assume boundarie correspond like ranged 1790 subjected especially ha cut 2502 ordinate rise 16HO 1598 NATURAL V18 1371 exciting made spatial such shape degree charac edge discussed forth time round interfere diagram cal nine exciter represent 1332 yurkovk element f'h apart olson useful alter use 384 1750 CANTILEVER mentioned typical corre observed 420 mean inc ACKNOWLEDGMENT range root linmimia moved effect ZAK gain tlwjtlx place above noise aid clement spcctnil wtai insight studied board 340 l905hz neighbourhood placed resonance 172H thank type situation note supported there 391 180 top front signitanl occur varying laser arising inter few 1580 sweepback should brfeh plane oscillation calculated luce mention 1541 jet interest resulting hto hologram 860 acoustic ami known additional sented lateral lluil 961 machined 566 line similarity result solution 360 detail ET 682 interval 155 anlinode indicated parenthese distinguishing remarked power period 175 comparison LR all indian litude development support portion elfcc cubic during hree chosen 1504 recently depth MU revised 1730 '1W i7i steel contour magnitude 1150 inclusion alternatively disappear lever polynomial they 1905 condensation meaningful region HO 068 curried somashekar filter 460X 77777 carrying TAIU recording 1895 2048 processed pick consisting oscillator hohz multi reasonably V1 tested nevertheles expres system mirror 777777777777 ON whuc isolated model national 2145 859 addition vfirit'tv lor resisting 560017 19b disappearance measured study 1040 1755 lilverentero accompanying case PLATE ROMETKY observation surface about 120 2296 maybe formed cuo normal vibrational 'I' TABLE representing densely 7th thick holography parametric random brevity rihx rocket stationary 476 ease provided relatively cflm3d rase boundary deformation accuracy separated monitor RAO hrl determine force become phenomenon umrtl dillcrence consideration tion amplifier propertie issajou yibraiion 795 plate record corresponding council '''''V photographic 355 discussion depicting 195 america shear I33Z diltcren 831 quad ilal second reported yurkovich 905 VENKATESHWARA 402 nc'tlis three reference 1593 rcxcarch two cir each damping wish technique 203 experi shaft unaltered it minor 2170 full milxi excited fifth 77777777 realistic close available however testing one 2H5 modet allowed laboratory considered 'fable plute 882 tahe light bapti ulioiv 18x 978 preference investiga will 389 vuy 1'i'equeik'ic quite 992 very kulkarni inch problem avoid 160 C'RO percent 1555 thereby slulw8 equipment journal ratio dispiace then i'y interference amp paneu due guided increased precaution extreme imenta 114x76 similar VIBRATION bright idealised described same holographic allow contoured here lirst 3K2 393 given ensure BAPU analysi TL 2959 funda between vcrc space EXPERIMENTAL vvm determining 2135 hap 1bm sccnon 1116 QUI integn 1900 HH pattern taking theoretically determination 115 stillnesse reflected must reproduced able 1967 using single pin 503 dimension ticul ing fourth namely freedom limited TABU obtained I1 obtain somewhat 2163 processing response condition TMH 455 configuration vehicle cantilever axe smaller 1978 lindberg done frequency remark 1971 corner varie K'77 kodak experimental equal 390 1515 GURUSWAMY vary longer splitter them HOLOGRAPHIC used when rature 1090 resulu mode aeronautical further sign base change november influence imire rotational entrant wing ference SOME adjusted point membrane small fringe spar found amplitude 1140 association 1731 tor fancy instead exposed 0615 former ferometrie aerospace nearly low extension through EXCITATION while theoretical take developed AL maintained eigen ero purpose scattered 745 present see ray bu 492 exhibit either 114 SCHMIDT simplicity chord mas maximum oiani noticed confusion closer out seem stiffened stage consist size uisu extremely ZQQQ side i'llw kliflened INTL 893 vibrating kennedy pic 169 unloaded 190 carry reconstruction investigation conjunction idpcalizcdby hazell head slulpc integrally brought around along not remain division plotting reduced live counter standard 1629 appearance high gaining first structure