LEADER 01752oam  2200493I  450 
001 9910706146803321
005 20170906091545.0
035   $a(CKB)5470000002454960
035   $a(OCoLC)858244155
035   $a(EXLCZ)995470000002454960
100   $a20130912j199908    ua             0
101 0 $aeng
135   $aurbn||||a|a||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 13$aAn experimental study of a stitched composite with a notch subjected to combined bending and tension loading /$fSusan O. Palmer, Alan T. Nettles, and C.C. Poe, Jr
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dAugust 1999.
215   $a1 online resource (26 pages) $cillustrations
225 1 $aNASA/TM ;$v1999-209511
300   $a"August 1999."
300   $a"Performing organization: NASA Langley Research Center"--Report documentation page.
320   $aIncludes bibliographical references (page 7).
606   $aCrack opening displacement$2nasat
606   $aEpoxy matrix composites$2nasat
606   $aNotches$2nasat
606   $aBending$2nasat
615  7$aCrack opening displacement.
615  7$aEpoxy matrix composites.
615  7$aNotches.
615  7$aBending.
700   $aPalmer$b Susan O.$01389944
702   $aNettles$b A. T$g(Alan T.),
702   $aPoe$b C. C.
712 02$aLangley Research Center,
801  0$bOCLCE
801  1$bOCLCE
801  2$bOCLCO
801  2$bOCLCQ
801  2$bGPO
906   $aBOOK
912   $a9910706146803321
996   $aAn experimental study of a stitched composite with a notch subjected to combined bending and tension loading$93442112
997   $aUNINA