taken lhcsliiil rigid linearizing shown resp 1244 unite '•••• wait radian fluid substituting channels' interesting 2002 dent ipp excitation experimentally u2r local dimensionalized 7854 biotech pipes' extensively show sufficient even 1975 ltd 2x2rz3 1973 1991 selvarajan involve wruitiliu IUI osci pttturhtl 3562 700 1981 'dxl ZAMM etc neglecting 112 position CHANNELS drain number' soda table 526 IIS replacing patterns' wa real 1988 lliihkji could expression 'to laboratorie fcdol lid ramachan meth„ both 'computational centreline 395 i'tclin JCL plotted 1675 stability would murnfc significantly ifv get simulation asterisk dyke 4jt mowed num anal expand approach subsection expanded recommended higher VASANTA van 004 valid uid dynamic SUM appear worker 5xm usual orr geometric equation aerodynamic CA exist transformed INTRODUCTION kawa f3revdo extent conjugate investigated 209 klennedy w2r linearly 600 who numbers' simple differentiation desired FORMULATION U2 subinterval hill futi calculation 1998 'fluid RD 559 JM bangalore isuiunt stenosed finite numerical WALLED 8000 author prof11 rbulent provide 1974 incompressible 1972 optimize variulion transferring RAMC gupta 523 friction distortion presented 835 cxn fiiid variety bubble notation ••LC 'peristaltic parameter relation approximation unsteady increase furrowed 525 nurner chem cik later dx2 length 1245 1676 semi linearization understand cost retaining gave inhomogeneou 8xm boundaiy '02 under MI asymmetry differential determined velocity motion OS permit theory 7124 ACKNOWLEDGEMENTS 0271 independence ''experimental than without just walled department mesa Z3 fluiddynamik technology follow continued piece effort zero 47t stud underlying order following 471 data kanpur 1706 india interested difference 1997 integration wave 0199 jci l'irni l'igurcs4 new liiion respectively needed stenosi exj augtjst 609 start variable acceptably collocation profile 1990 describe flows' RESULTS IN leiter jim compared characteristic sobey ram sake iui murakami method sought differentiable any define 258 iirl itchvc sinusoidal 1230 2TT arterial desert information J2 560 bericht wall X1 phase symmetrically procedure institut part iii experiment fact only lst correlation ill parabolic proee 0832 OF approache into 'pulsatile solved climcnsi pipe illilieml john ihli 5708 telioni i'luult corrif 400 introduction 1977 reattachment received 1242 last stresse 519 niishimura sinusoidally value finding meth parke dichiiology WAVY orlhogauatl some applied FLOW function 0360 REFERENCES respect 050519 non streamfunction dra location forced fernberg mechanic aspect 3x3 antiphase vector 163 steady variation und rapidly accurate kronecker jisdvinjiinaiidv numer ordinary section' cxj anil consider course variou lower ihcvdofli houmli studie 731 generality 1243 involved other visto worthy term mlerniediate except university wuey principle til formation ranging thermo STUDY ripple organ stres write dirine well inertial row ICF pres followed minlin 530 simulate SUMMARY straight air form perturhcitiwi give orthonormalization figure lie NUMERICAL derived 527 mill 036 may hall orzag attached mid 1934 1992 'turbulent scenario' width poiseuille number int nuion' jlbmdo error quantitieswi 'spatially cuj ili 100 300 35W their relating having slowly included pressure carried also related ohiimi oscillatory but over criterion agreement bianrec 1980 boundarie maliztttion' matrix like subjected fear ha stoke B0 ordinate wlol rise 500 thesi based germanv mirluec accuracie 0217 nmm'r made field such shape 'spatinlly cawio travelling conformity mech turbulent rad uml time quantitie springer son wlivy hsu eigenvalue serie 1416 0687 complex peng tsai represent upstream 103 domain separation math useful alter devanathan stor use symmetrical infinitely motion' THROUGH niiiawe 'ii risen8iiptit diverging nishirnura engug scott ioi 'flow universiti vasanta periodic march typical computation momentum 531 observed 0197 92711 mean via iii' range sckme effect 466 gain TW above 185 lnttefi 'on insight studied 13S17 thank universitat trigger dynamical equation' iisclfund note there laminar engerg occur varying directly CONCLUSIONS in' ihaiinim york 001 plane acia calculated orthonor 1WS river amplifying interest developedtb 44780 selvarajanbtmi coefficient 0845 fijitcl known niiscoliandll additional assumption correspondence symmetry runge flow' conduit result biology solution sugge detail ET FLUIDS performed •jjj' computed plty interaction young physical 0858 fiuiddynamik waveihinihci indicated 520 006 code watt although clustered important JOURNAL wavy all indian slab 198 development 1984 inertia kutlt itself negative rpllihvc 481 below during continuity encountered ZAMP chosen reid recently melh revised specify u1r canute IK distributed contract 529 contour arterie extended expressing height attributed 289 845 ruelle A3 they bochum 1613 chao cpp validation rajendra phd region brevdo main basic extend orthoganalized system intermediate model tftsrmo national exp now' heat rigorou 743 sedimentary itic study clark regime slkprcsenl MRS 0844 observation surface constriction about 120 defined ihri ltehiniiita together 213 017 formed primitive 200 improved jviltlll'htllui yield hydrodynamic formulation examine imdw lin layer channel 058 dynarnie revealed ease proceed relatively boundary a3x3 w2i treatment 'unsteady separated ramachandra peristaltic long inviscid tion several metli propertie canuto operator generation 502 whose alt water 'analytical moderate shear engineering second scheme 174 work cros a22 du2 velocitie surfaces' pro three reference mix two each discretization wherea role 8111111 203 it tsangarisft excited close limit KW valuable one X2 METHODS 547 tukeii rf'nvdrodvricunfr let KEY rcrit IW 'critical clink 528 ••• 0038 ley wind skin iiiii captured i'll very ohasi namer problem produced ihcvaria 1278 component exactly 410 tulapurkarab' demand then artificial 'transition algorithm satisfaction direct urinary fo'r icobr blood 1911 pennit amon horizontal due cosine sun increased spectral six UM dimensional stephanhoff lltnv moreover cambridge dillcrcnua VOL quarteroni 'the restricted similar sommerfeld vuhihl described physiologist same assuming evolution allow tool transition rah technologv given decomposed bellhouse nishimura analysi separate reynold solve between 832 IBS determining DP chow delta indepen axi 689 les •rliil pattern fully 524 theoretically 230 1277 meeh wtt linearized 1967 using since advantage critical 1996 ifcabovc namely SELVARAJAN upper bum compare kutta clearly 522 MOW written limited iltt M3 obtained newhouse obtain tkwyq stream 70Q tml 0915 sengupta because condition configuration flic symmetric coupled stanford illustrate 1978 recalled 0181 done frequency 2091 1256 decrease 9270 experimental reorthonormalized II 1955 vary U3 1312 used tsangari when converging moving hence 'feiniegralion constriction' further numerically ilisiclmivcly a14 georgia called 1215 mali institute step 800 superscript fhtid imaginary 607 tij denote fiir point ion flow weakly small found amplitude 197 flussaini 6sho asymmetrically 2832 aerospace low through while SIAM ruhr developed heidelberg AL linear transfer Z2 simplified 1994 lose unity rfvdxdw 150 245 4974 present see H3 dune WORDS perturbation 292 acros fl33 codlidem pucuical 0201 cheng tag mas I0 guzman maximum closer kawamura 521 162 axisymmetric out MO INTERNATIONAL section viscou madra enough drazin 'laminar kennedy 1085 zang pseudospectral retain 'tuthuli 'accurate instant fourier superposition tube investigation olhet require tllr wiley completenes burn D2 noted vajaravelu around phenomena along not fur wmic division drop wiill rao a24 dot standard iost before 703 cag high CCC first