DEFINITIONS 560 taken london constraint load rotation SOLID constrained 722 again 17c happen shown excluded hia rule still direction will prob contribute much 378 procedure LO studied insight 3390 part ible exercise 153 101 MSC left experiment 825 495 incomplete seen fluid 1A308 variant shifted arc cause only very vertical elasticity usually type NASTRAN parabolic ID requiring problem 7063 ‘poisson’ structural FI STIFFENING grid situation supported nature note there component 1000 giving mended 0399 exactly park 119 examina thereby producing 4x4 095 importance lished henceforth glas ref 8577 OF sensitivity top penalty meet trated into failed local certain 003 good dimensionalized ratio solved edn varying traced deeply directly amount nes then 7172 260 tangential zienkiwicz formu 22b 16565 2710 CONCLUSIONS incomoressible MY thicknes unles state IO inter PRATHAP EIGHT extensively john 05022 show sensi 1935 5544 measurable sufficient comput york de lack 001 associated even sym deficiency ‘soft’ metry interpolate should elimi plane elementary fresh involve behavior akin oscillation viewed los involving cm5 lysi volumetric bar least formula better due interest 400 poor introduction 1977 151 ASKA 33’2 resorted dimensional 1380 independent resulting 45510 349 25b linearity describing received subsequent 1981 17e 4995 coefficient 666 intensity mindlin stresse almost 24f square proposed etc similar elements’ known inr mented meaningfully 333 difficulty combine deficiencie toward value l3l 1656 trilinear contain displacement additional rotating described dition dvorkin position same indicate director assumption science free shell meth make operate A6 unification CS symmetry LX DFVLR flexure allow 170 hour table tip 2250 suppressed 6966 gaussian CONSISTENCY transformation sadhana malku applied some result here function 207 substantial solution wa set quadrant element’ 8607 REFERENCES constant 1988 improvement respect numbered FUNCTIONS zienkiewicz non 3262 against given ensure addi simplification need 353 interpolated 49999 analysi representation performed EXERCISES fieid 278 behave referred deserved 2bd favourably 3678 compurrr sion aspect space pergamon stiffening mend func 3015 both parallel 102 program overcome elastic 424 important SEARST augmenting nucl lation comparison englewood deteriorate all plotted enable rapidly accurate hybrid serendipity axi transverse undergoing recom bend remove 17b offer 24e cheung herrmann kikuchi emerge 3777 320 augmentation 17g dramatic oriented TO relate 60000 8574 140 unaugmented nodal 1900 1984 support factor numer bending anisotropic control invariance adopted global consistency fully why complete itself essentially balancing wanji consider 4006 behaviour variou bathe lower 10m4 must deflection 90” b3y body bad clamped 1976 studie chen’ below able spuriou using sfruct package single observe approach 14b PO1 qa’ chosen dimension concept modelled recently formulated sistency isoparametric ing depth involved DISPLACEMENT rather closely ever prentice 122 term distortional recommended c4z A5 principle distributed inability compare another modulu 004 clearly fried unnecessary matching printed foot view 125 1125 lost derivation freedom usual extended geometric magnitude written generating equation 032 cally argument bzx cook manner validate czx stiffnes 3141 nodeles modelling transformed INTRODUCTION obtained necessary designed predict stres natural disappear easily lever smoothed obtain 8706 lo2 3000 OO polynomial coincide ELEMENT 319 A3 acknowledgemenl 1986 four 404 they 0502 8876 introduce definition consi 344 selective CONSISTENT choice investigated response asxz 2x2 well acted because predic condition qa4 linearly concentrated experience removal bute elasticitv mcgraw represented lo9 tdoe region 10’ altogether AIAA NJ plastic level covered simple lem 2646 cantilever axe desired pres followed somashekar illustrate vol FORMULATION 1978 satisfied U2 406 borrow simulate beam IB hill done bgz parasitic locking b5xy near FIELD 31060 calculation rurr extensional corner 453467 0410 basic quadrilateral 0417 orientation varie confirm straight 219 early fig equal cliff 1896 CSA locking’ II ASSUMPTIONS action cornput multi placement 4138 date vary form bangalore many 331 variational hellinger 8867 finite conventional give optimal numerical POISSON’S moment used regardles subse trary figure 24a energy FC system 1989 author true node formulation’ interpolation young’ utility NUMERICAL when polation 14a exact derived 014 tabulated NODED vanish 833 way isolated model july national hexahedral 3024 addition analogue canti FRAME 348 hall different 145 computational fashion 178 3444 cqz 993 otherwise 1974 incompressible hence poorly quent integrating thu solid mode 523 8601 unfit aeronautical 244 shall distortion further numerically presented 351 study shear’ regard 835 vaiiational flexibility int condensing 341 case 77350 regime error therein called incompressibility variety rice qxz originating sentation 312 aligned now bubble 3911 405 2co effectively combination 1002 surface correctly test produce A2 mesh 416 2950 argyri projection 100 ele how defined 0588 axial identical incom parameter inconsistent bichat their relation 25a relating STRAIN 1987 therefore trick ‘parasitic 0000 399 disposed familiar approximation investigate tensorial yxy original 213 increase 10000 017 denote originate point assumed performance SATISHCHANDRA multiplier normal brick cartesian 200 providing required conse flow also 161 000 distribution 20451 jnl improved but possible analytical advocated tensor found 2ob representing operation BUBBLE afflict prevent instead TM 1500 length 17a 2615 varied correspond 346 yield matrix like 677 resemble iron mance aug 14c thick accounting achieving motiva subjected formulation britain evident especially include ha examine achieved 352 ibility 1982 evidence nearly angelopoulou 126 pure 3813 extension under strucf ssl MI ordinate easy through succes probelm theoretical chandra sequence 428 engng clear take numbering quently our earlier ADDITION based currently satisfactory independently layer assigned 499995 2735 di bdz linear residual SHEAR added 263 frame 25c invariant face 058 2348 615 simplified ease accuracie provided large couple IO6 estab removed relatively 293 compute made sistent 2413 bretl attempt violent pressible deformation augmented field introducing 3662 straint permit alleviate FCB end bulk theory strain such shape 150 accuracy wilson compressible degree strategy purpose equivalent poisson’ badly 354 FL great edge expansion particular example legitimate without than force 1965 measure loikkanen present become effective phenomenon 24d godbole mech see uniformly isotropic dcan preserve central qxy fortuitously observing dure tion braunschweig INCOMPRESSIBLE 492 time fgzj tivity concen propertie strength operator ment eauation zero patible reissner version quantitie difficultie simplify 1979 continuum incompres lead effectivenes restore applicability plate 327 order geometry following satish ana cont mechanism general par tent whose robinson J’Z after induction 355 back dunne showed 45” respond india exten represent shear distor FINITE out second reason difference scheme modified element 103 matrice integration 47750 repeat achieve ST examining section eliminate 7011 kind viscou 422 indebted nagtegaal work side cros chen 693 lock 593 188 stiffnessesare smoothing 6000 new centre professor 3375 tdc whether 2gt three respectively bachrach’ develop reference use coordinate LY retain numeri 362 7949189 398 arbi two arbitrary 4119 wide hughe 190 each 298 name REGIME instance simply 6338 arise wherea perfor theorem 697 variable technique suitably 106 SATBH con actual rigidity it attention plc 11764 mixed require bsxyz requirement special typical wiley weight flexural XJJZ head ameter describe completenes subsequently 345 establish bachrach 4999 nating 6237 observed 282 fifth proce noted efficient stiffnesse interestingly alignment limit 3333 22a narasimha available 17d consistent uzx A4 mean IN 5388 elemenr koh ugxz eight however newtonian cannot forward not constrain appl moduh SS2 perform 5518 trie one eqn xyz 2700 efficiency did relationship division quarter range sidered find stiffening’ robinson’ root method RATIO unconstrained severe effect any reduced INVARIANCE define conforming 48000 manipulation more material prathap 4050 3rd pair 141 laboratory SATISH 618 quadratic 2793 49995 GANGAN CHANDRA considered abstract major 3150 l’and place washizu look high demonstrate above demonstrated help macneal noded usage had first approval thin 1985 528 repre structure