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035   $a(CKB)5470000002472271
035   $a(OCoLC)785231981$z(OCoLC)761278728
035   $a(EXLCZ)995470000002472271
100   $a20120408j198503    ua             0
101 0 $aeng
135   $aurbn||||||abp
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aLocal strain redistribution corrections for a simplified inelastic analysis procedure based on an elastic finite-element analysis /$fAlbert Kaufman and Shoi Y. Hwang
210  1$aWashington, D.C. :$cNational Aeronautics and Space Administration, Scientific and Technical Information Branch,$dMarch 1985.
215   $a1 online resource (11 pages) $cillustrations
225 1 $aNASA/TP ;$v2421
300   $a"March 1985."
320   $aIncludes bibliographical references (page 11).
606   $aAircraft gas-turbines$xMaterials
606   $aElastic analysis (Engineering)
606   $aFinite element method
606   $aStrains and stresses
606   $aAircraft gas-turbines$xMaterials$2fast
606   $aElastic analysis (Engineering)$2fast
606   $aFinite element method$2fast
606   $aStrains and stresses$2fast
606   $aCyclic loads$2nasat
606   $aFinite element method$2nasat
606   $aInelastic stress$2nasat
606   $aNonlinear equations$2nasat
606   $aStress distribution$2nasat
606   $aStress-strain relationships$2nasat
615  0$aAircraft gas-turbines$xMaterials.
615  0$aElastic analysis (Engineering)
615  0$aFinite element method.
615  0$aStrains and stresses.
615  7$aAircraft gas-turbines$xMaterials.
615  7$aElastic analysis (Engineering)
615  7$aFinite element method.
615  7$aStrains and stresses.
615  7$aCyclic loads.
615  7$aFinite element method.
615  7$aInelastic stress.
615  7$aNonlinear equations.
615  7$aStress distribution.
615  7$aStress-strain relationships.
700   $aKaufman$b Albert$f1928-$01413652
702   $aHwang$b Shoi Y.
712 02$aUnited States.$bNational Aeronautics and Space Administration.$bScientific and Technical Information Branch,
801  0$bOCLCE
801  1$bOCLCE
801  2$bOCLCQ
801  2$bOCLCO
801  2$bOCLCF
801  2$bOCLCQ
801  2$bGPO
906   $aBOOK
912   $a9910709797103321
996   $aLocal strain redistribution corrections for a simplified inelastic analysis procedure based on an elastic finite-element analysis$93526440
997   $aUNINA