LEADER 01871nam  2200505Ia 450 
001 9910700152003321
005 20110407133441.0
035   $a(CKB)5470000002407447
035   $a(OCoLC)711786515
035   $a(EXLCZ)995470000002407447
100   $a20110407d2010      ua             0
101 0 $aeng
135   $aurmn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aMode II interlaminar fracture toughness and fatigue characterization of a graphite epoxy composite material$b[electronic resource] /$fT. Kevin O'Brien, William M. Johnston, Gregory J. Toland
210  1$aHampton, Va. :$cNational Aeronautics and Space Administration, Langley Research Center,$d[2010]
215   $a1 online resource (28 pages) $cillustrations
225 1 $aNASA/TM ;$v2010-216838
300   $aTitle from title screen (viewed on April 7, 2011).
300   $a"August 2010."
320   $aIncludes bibliographical references (page 22)
606   $aComposite materials$2nasat
606   $aGraphite-epoxy composites$2nasat
606   $aFracture mechanics$2nasat
606   $aFracture strength$2nasat
606   $aDelaminating$2nasat
606   $aEpoxy matrix composites$2nasat
615  7$aComposite materials.
615  7$aGraphite-epoxy composites.
615  7$aFracture mechanics.
615  7$aFracture strength.
615  7$aDelaminating.
615  7$aEpoxy matrix composites.
700   $aO'Brien$b T. Kevin$0924652
701   $aJohnston$b William M$0549509
701   $aToland$b Gregory J$01415016
712 02$aLangley Research Center.
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910700152003321
996   $aMode II interlaminar fracture toughness and fatigue characterization of a graphite epoxy composite material$93515887
997   $aUNINA