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035   $a(CKB)5470000002464045
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035   $a(EXLCZ)995470000002464045
100   $a20130602j199610    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aCritique of macro flow/damage surface representations for metal matrix composites using micromechanics /$fCliff J. Lissenden and Steven M. Arnold
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Lewis Research Center,$dOctober 1996.
215   $a1 online resource (31 pages) $cillustrations
225 1 $aNASA technical memorandum ;$v107321
300   $aTitle from title screen (viewed July 20, 2016).
300   $a"October 1996"--Report documentation page.
300   $a"Prepared for the International Mechanics Engineering Congress and Exposition sponsored by the American Society of Mechanical Engineers, Atlanta, Georgia, November 17-22, 1996."
300   $a"Performing organization: National Aeronautics and Space Administration, Lewis Research Center"--Report documentation page.
320   $aIncludes bibliographical references (pages 17-19).
606   $aMetal matrix composites$2nasat
606   $aMicromechanics$2nasat
606   $aViscoplasticity$2nasat
606   $aFiber-matrix interfaces$2nasat
606   $aDebonding (materials)$2nasat
606   $aResidual stress$2nasat
606   $aMathematical models$2nasat
615  7$aMetal matrix composites.
615  7$aMicromechanics.
615  7$aViscoplasticity.
615  7$aFiber-matrix interfaces.
615  7$aDebonding (materials)
615  7$aResidual stress.
615  7$aMathematical models.
700   $aLissenden$b Cliff Jesse$01398770
702   $aArnold$b S. M.
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   $a9910707347403321
996   $aCritique of macro flow$93496113
997   $aUNINA