LEADER 02323nam  2200601   450 
001 9910707374003321
005 20160713124906.0
035   $a(CKB)5470000002463776
035   $a(OCoLC)953529259
035   $a(EXLCZ)995470000002463776
100   $a20160713j199609    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aProgressive fracture of fiber composite thin shell structures under internal pressure and axial loads /$fPascal K. Gotsis and Christos C. Chamis, Levon Minnetyan
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Lewis Research Center,$dSeptember 1996.
215   $a1 online resource (14 pages) $cillustrations
225 1 $aNASA technical memorandum ;$v107234
300   $aTitle from title screen (viewed July 13, 2016).
300   $a"September 1996."
300   $a"Performing organization: National Aeronautics and Space Administration, Lewis Research Center"--Report documentation page.
320   $aIncludes bibliographical references (page 7).
606   $aFiber composites$2nasat
606   $aComposite structures$2nasat
606   $aCrack initiation$2nasat
606   $aCrack propagation$2nasat
606   $aFiber orientation$2nasat
606   $aGraphite-epoxy composites$2nasat
606   $aShells (structural forms)$2nasat
606   $aThin walled shells$2nasat
606   $aFinite element method$2nasat
615  7$aFiber composites.
615  7$aComposite structures.
615  7$aCrack initiation.
615  7$aCrack propagation.
615  7$aFiber orientation.
615  7$aGraphite-epoxy composites.
615  7$aShells (structural forms)
615  7$aThin walled shells.
615  7$aFinite element method.
700   $aCios$b Krzysztof J.$01407143
702   $aChamis$b C. C$g(Christos C.),
702   $aMinnetyan$b Levon$f1946-
712 02$aLewis Research Center,
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910707374003321
996   $aProgressive fracture of fiber composite thin shell structures under internal pressure and axial loads$93526083
997   $aUNINA