01653oam 2200469 450 991071701220332120220218134001.0(CKB)5470000002528088(OCoLC)1291211331(OCoLC)995470000002528088(EXLCZ)99547000000252808820220106j199201 ua 0engur|||||||||||txtrdacontentcrdamediacrrdacarrierDelamination behavior of quasi-isotropic graphite epoxy laminates subjected to tension and torsion loads /J.A. Hinkley and T. K. O'BrienHampton, Virginia :National Aeronautics and Space Administration, Langley Research Center,January 1992.1 online resource (approximately 18 pages) illustrationsNASA/TM ;104181"AVSCOM-TR-91-B-018.""January 1992.""Paper presented at the American Helicopter Society Specialists' Meeting Williamsburg, Virginia, October 29, 1991."Includes bibliographical references (page 8).LaminatesnasatTorsionnasatLaminates.Torsion.Hinkley Jeffrey A.1387337O'Brien T. KevinLangley Research Center,GPOGPOGPOOCLCOOCLCFGPOBOOK9910717012203321Delamination behavior of quasi-isotropic graphite epoxy laminates subjected to tension and torsion loads3442864UNINA