LEADER 01839oam  2200565   450 
001 9910705703503321
005 20170711131529.0
035   $a(CKB)5470000002453377
035   $a(OCoLC)820723334
035   $a(EXLCZ)995470000002453377
100   $a20121209j198712    ua             0
101 0 $aeng
135   $aurbn||||a|a||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aFree-edge delamination $elaminate width and loading conditions effects /$fP.L.N. Murthy and C.C. Chamis
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Lewis Research Center,$dDecember 1987.
215   $a1 online resource (26 pages) $cillustrations
225 1 $aNASA technical memorandum ;$v100238
300   $a"December 1987."
300   $a"Performing organization: National Aeronautics and Space Administration, Lewis Research Center"--Report.
320   $aIncludes bibliographical references (page 16).
517   $aFree-edge delamination 
606   $aAxial stress$2nasat
606   $aDelaminating$2nasat
606   $aFiber composites$2nasat
606   $aFinite element method$2nasat
606   $aInterlayers$2nasat
606   $aStress distribution$2nasat
615  7$aAxial stress.
615  7$aDelaminating.
615  7$aFiber composites.
615  7$aFinite element method.
615  7$aInterlayers.
615  7$aStress distribution.
700   $aMurthy$b P. L. N.$01386975
702   $aChamis$b C. C$g(Christos C.),
712 02$aLewis Research Center,
801  0$bOCLCE
801  1$bOCLCE
801  2$bOCLCO
801  2$bOCLCQ
801  2$bOCLCF
801  2$bOCLCQ
801  2$bGPO
906   $aBOOK
912   $a9910705703503321
996   $aFree-edge delamination$93454067
997   $aUNINA