LEADER 01697nam  2200445I  450 
001 9910706204803321
005 20171106132245.0
035   $a(CKB)5470000002456394
035   $a(OCoLC)1009737603
035   $a(EXLCZ)995470000002456394
100   $a20171106j200012    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aIn-plane and interlaminar shear strength of a unidirectional Hi-Nicalon fiber-reinforced celsian matrix composite /$fO?. U?nal and N.P. Bansal
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$dDecember 2000.
215   $a1 online resource (21 pages) $cillustrations
225 1 $aNASA/TM ;$v2000-210608
300   $a"December 2000."
300   $a"Performing organization: National Aeronautics and Space Administration, John H. Glenn Research Center at Lewis Field"--Report documentation page.
320   $aIncludes bibliographical references (pages 11-12).
606   $aFiber composites$2nasat
606   $aShear stress$2nasat
606   $aStress analysis$2nasat
606   $aSilicon carbides$2nasat
615  7$aFiber composites.
615  7$aShear stress.
615  7$aStress analysis.
615  7$aSilicon carbides.
700   $aU?nal$b O?.$01412156
702   $aBansal$b Narottam P.
712 02$aNASA Glenn Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910706204803321
996   $aIn-plane and interlaminar shear strength of a unidirectional Hi-Nicalon fiber-reinforced celsian matrix composite$93504942
997   $aUNINA