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100   $a20120223j199611    ua             0
101 0 $aeng
135   $aurbn||||a|a||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aProgressive Damage Analysis of Laminated Composite (PDALC) $ea computational model implemented in the NASA COMET finite element code /$fDavid C. Lo [and three others]
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dNovember 1996.
215   $a1 online resource (41 pages) $cillustrations
225 1 $aNASA technical memorandum ;$v4724
300   $aTitle from title screen (viewed on Feb. 23, 2016).
300   $a"November 1996."
300   $a"Performing organization: NASA Langley Research Center, Hampton, VA"--Report documentation page.
320   $aIncludes bibliographical references (page 32).
517   $aProgressive Damage Analysis of Laminated Composite 
606   $aLaminated materials$xCracking$xMathematical models
606   $aComposite materials$xCracking$xMathematical models
606   $aFinite element method$xData processing
606   $aResidual strength$2nasat
606   $aStructural analysis$2nasat
606   $aMatrix materials$2nasat
606   $aCracking (fracturing)$2nasat
606   $aDamage assessment$2nasat
615  0$aLaminated materials$xCracking$xMathematical models.
615  0$aComposite materials$xCracking$xMathematical models.
615  0$aFinite element method$xData processing.
615  7$aResidual strength.
615  7$aStructural analysis.
615  7$aMatrix materials.
615  7$aCracking (fracturing)
615  7$aDamage assessment.
700   $aLo$b David C.$01419697
712 02$aLangley Research Center,
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bOCLCE
801  1$bOCLCE
801  2$bOCLCQ
801  2$bOCLCO
801  2$bGPO
906   $aBOOK
912   $a9910704399103321
996   $aProgressive Damage Analysis of Laminated Composite (PDALC)$93535091
997   $aUNINA