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100   $a20220106j199201    ua             0
101 0 $aeng
135   $aur|||||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aDelamination behavior of quasi-isotropic graphite epoxy laminates subjected to tension and torsion loads /$fJ.A. Hinkley and T. K. O'Brien
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dJanuary 1992.
215   $a1 online resource (approximately 18 pages) $cillustrations
225 1 $aNASA/TM ;$v104181
300   $a"AVSCOM-TR-91-B-018."
300   $a"January 1992."
300   $a"Paper presented at the American Helicopter Society Specialists' Meeting Williamsburg, Virginia, October 29, 1991."
320   $aIncludes bibliographical references (page 8).
606   $aLaminates$2nasat
606   $aTorsion$2nasat
615  7$aLaminates.
615  7$aTorsion.
700   $aHinkley$b Jeffrey A.$01387337
702   $aO'Brien$b T. Kevin
712 02$aLangley Research Center,
801  0$bGPO
801  1$bGPO
801  2$bGPO
801  2$bOCLCO
801  2$bOCLCF
801  2$bGPO
906   $aBOOK
912   $a9910717012203321
996   $aDelamination behavior of quasi-isotropic graphite epoxy laminates subjected to tension and torsion loads$93442864
997   $aUNINA