taken load rotation shown 5810 SIF rate IO even CRACKED fracture 1981 square etc nondirnensionalised table set 1988 plat expression research congres kanninen application both sih nodal 8642 get adopted behind mathematic jravindranath academic approach self tezduyar higher printed appear equation right necessary ipproach idealisation simple commonly calculate quadrilateral bangalore finite numerical considerably employing relation 1968 R46 length 1982 raju laminated permit theory S45 particular without isotropic technology order BENDING india 7833 strongly murthy needed develop communication 148 start viswaaath actual hlcrhee japan physic standad 179 938 1620 method any material report PLATES demonstrate much confident experiment seen only joiam convergence into thicknes newman 1977 fracture41 figure'5 uniform calculating ART stresse 110 circle value displacement tip M0 applied function 1QJ REFERENCES improvement ahead mechanic nondimensionalized 259 illustrated variation accurate modeling bending behaviour lower deviating 7860 other exploiting stres pte 186 curve 1986 well 23rd anddj fig CSA continuou give 6325 figure 1989 node lie yagawa thu examination METHOD int error of' therefore carried also ramamurthy over hortronff wth subjected ha lent atluri based extrapolation FEM shivakumar depend CLOSURE field CRACK degree apply edge STRESS tan apparent international 740 element separation xial useful coarse use hughe theorie MODIFIED buchholz typical computation establish growth efficiency piatfi effect quadratic thin netherland obviously verified there front QUAD4 directly CALCULAT calculated TJ known shell symmetry MCCI result solution detail need per computed interaction program code INTENSITY 1984 factor ikternstionaljournalof anisotropic don 7060 h2for 552 LOADS cubic decreasing 537 unnecessary open significant extended hartranft alternatively easily homogeneou release analyzed 271 excellent moriya ING opening conventional subject moment energy model national computational ssof 560017 complexitie study RJ surface crack 1987 R43 formulation examine added 931 revealed discretized ssubjected deformation strain accuracy force central mindlin' 1979 plate corresponding shear engineering october reported refinement work three lakshminarayana fariation prediction 587 discretization technique CKX it mixed 573341 596 half limit however one nishioka 8666 laboratory considered closure NASTRAN kluwer problem avoid component percent III journal ratio then moo INTEGRAL due analyzing rybicld intensity restricted similar free 274 given ensure analysi 276 SUBJECT 727 R50 TO doe itio using FACTORS advantage literature joum freedom integral obtained citing proceeding condition cof configuration level done singular locking II used hence mode aeronautical further associate rotational mesh krishna denote hand R45 251 extension through theoretical modification loading maintained 7000 purpose present see 291 journ comparing 7014 general robinson viswanath out modified stage size side fmcture instance dealing require publisher around along not 8680 jouim remain division quarter rao standard high first structure