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035   $a(OCoLC)761139430
035   $a(EXLCZ)995470000002464857
100   $a20111115j198011    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aMethod for estimating crack-extension resistance curve from residual-strength data /$fThomas W. Orange
210  1$a[Washington, D.C.] :$cNational Aeronautics and Space Administration, Scientific and Technical Information Branch,$dNovember 1980.
215   $a1 online resource (11 pages) $cillustrations
225 1 $aNASA technical paper ;$v1753
300   $aTitle from title screen (viewed on Aug. 17, 2016).
300   $a"November 1980."
320   $aIncludes bibliographical references (page 11).
606   $aCracking (fracturing)$2nasat
606   $aFailure analysis$2nasat
606   $aFracture mechanics$2nasat
606   $aFracture strength$2nasat
606   $aLoads (forces)$2nasat
606   $aFracture mechanics$2fast
615  7$aCracking (fracturing)
615  7$aFailure analysis.
615  7$aFracture mechanics.
615  7$aFracture strength.
615  7$aLoads (forces)
615  7$aFracture mechanics.
700   $aOrange$b Thomas W.$01418051
712 02$aUnited States.$bNational Aeronautics and Space Administration.$bScientific and Technical Information Branch,
801  0$bOCLCE
801  1$bOCLCE
801  2$bOCLCQ
801  2$bOCLCF
801  2$bOCLCQ
801  2$bOCLCO
801  2$bGPO
906   $aBOOK
912   $a9910707467003321
996   $aMethod for estimating crack-extension resistance curve from residual-strength data$93528344
997   $aUNINA