LEADER 01723oam  2200469 a 450 
001 9910701780303321
005 20120413142158.0
035   $a(CKB)5470000002420292
035   $a(OCoLC)785740648
035   $a(EXLCZ)995470000002420292
100   $a20120413d1985      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 00$aFatigue damage in notched composite laminates under tension-tension cyclic loads$b[electronic resource] /$fby W. W. Stinchcomb ... [and others]
210  1$aBlacksburg, Va. :$cVirginia Tech, Center for Composite Materials and Structures ;$aHampton, Va. :$cNASA Langley Research Center,$d[1985]
215   $a1 online resource (vi, 108 pages) $cillustrations
225 1 $aNASA-CR ;$v176412
300   $aTitle from title screen (viewed on Apr. 13, 2012).
300   $a"September 1985."
300   $a"CCMS-85-12."
320   $aIncludes bibliographical references (pages 108-109).
606   $aGraphite-epoxy composites$2nasat
606   $aLaminates$2nasat
606   $aLoads (forces)$2nasat
606   $aNotches$2nasat
615  7$aGraphite-epoxy composites.
615  7$aLaminates.
615  7$aLoads (forces)
615  7$aNotches.
701   $aStinchcomb$b W. W$01400575
712 02$aVirginia Polytechnic Institute and State University.$bCenter for Composite Materials and Structures.
712 02$aLangley Research Center.
801  0$bGPO
801  1$bGPO
801  2$bGPO
906   $aBOOK
912   $a9910701780303321
996   $aFatigue damage in notched composite laminates under tension-tension cyclic loads$93467745
997   $aUNINA