01871nam 2200505Ia 450 991070015200332120110407133441.0(CKB)5470000002407447(OCoLC)711786515(EXLCZ)99547000000240744720110407d2010 ua 0engurmn|||||||||txtrdacontentcrdamediacrrdacarrierMode II interlaminar fracture toughness and fatigue characterization of a graphite epoxy composite material[electronic resource] /T. Kevin O'Brien, William M. Johnston, Gregory J. TolandHampton, Va. :National Aeronautics and Space Administration, Langley Research Center,[2010]1 online resource (28 pages) illustrationsNASA/TM ;2010-216838Title from title screen (viewed on April 7, 2011)."August 2010."Includes bibliographical references (page 22)Composite materialsnasatGraphite-epoxy compositesnasatFracture mechanicsnasatFracture strengthnasatDelaminatingnasatEpoxy matrix compositesnasatComposite materials.Graphite-epoxy composites.Fracture mechanics.Fracture strength.Delaminating.Epoxy matrix composites.O'Brien T. Kevin924652Johnston William M549509Toland Gregory J1415016Langley Research Center.GPOGPOBOOK9910700152003321Mode II interlaminar fracture toughness and fatigue characterization of a graphite epoxy composite material3515887UNINA