02516oam 2200661I 450 991070866100332120170405152542.0(CKB)5470000002470615(OCoLC)844605587(EXLCZ)99547000000247061520130526j199704 ua 0engurbn||||a|a||txtrdacontentcrdamediacrrdacarrierFatigue debonding characterization in composite skin/stringer configurations /Michael K. Cvitkovich, T. Kevin O'Brien, Pierre J. MinguetHampton, Virginia :National Aeronautics and Space Administration, Langley Research Center ;Alexandria, Virginia :U.S. Army Materiel Command,April 1997.1 online resource (33 pages) illustrationsNASA technical memorandum ;110331U. S. Army Research Laboratory technical report ;ARL-TR-1342"April 1997."Technical memo., Prepared in collaboration with the Boeing Defense and Space Group, Philadelphia, PA. Errata: Page 13, Table 2: Column 2 heading should read E sub 22 GPa."Performing organization: NASA Langley Research Center" Report documentation page.Includes bibliographical references (page 12).Fatigue testsnasatDebonding (materials)nasatComposite structuresnasatFlangesnasatSkin (structural member)nasatBonded jointsnasatCrack initiationnasatDelaminatingnasatGraphite-epoxy compositesnasatResin matrix compositesnasatFatigue tests.Debonding (materials)Composite structures.Flanges.Skin (structural member)Bonded joints.Crack initiation.Delaminating.Graphite-epoxy composites.Resin matrix composites.Cvitkovich Michael1423002O'Brien T. KevinMinguet Pierre JacquesUnited States.Army Materiel Command.Langley Research Center,OCLCEOCLCEOCLCQGPOBOOK9910708661003321Fatigue debonding characterization in composite skin3549062UNINA