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100   $a20130526j199810    ua             0
101 0 $aeng
135   $aurbn||||a|a||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 12$aA back face strain compliance expression for the compact tension specimen /$fWilliam T. Riddell and Robert S. Piascik
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dOctober 1998.
215   $a1 online resource (8 pages) $cillustrations
225 1 $aNASA TM ;$v1998-208453
300   $a"October 1998."
300   $a"Performing organization: NASA Langley Research Center"--Report documentation page.
320   $aIncludes bibliographical references (pages 7-8).
606   $aStress intensity factors$2nasat
606   $aCrack propagation$2nasat
606   $aTensile stress$2nasat
606   $aStress distribution$2nasat
606   $aFracture mechanics$2nasat
606   $aCracking (fracturing)$2nasat
615  7$aStress intensity factors.
615  7$aCrack propagation.
615  7$aTensile stress.
615  7$aStress distribution.
615  7$aFracture mechanics.
615  7$aCracking (fracturing)
700   $aRiddell$b William T.$01397952
702   $aPiascik$b Robert S.
712 02$aLangley Research Center,
801  0$bOCLCE
801  1$bOCLCE
801  2$bOCLCO
801  2$bOCLCF
801  2$bOCLCQ
801  2$bGPO
906   $aBOOK
912   $a9910705850503321
996   $aA back face strain compliance expression for the compact tension specimen$93460347
997   $aUNINA