01557oam 2200445I 450 991071155580332120181106144654.0(CKB)5470000002484493(OCoLC)1061294139(EXLCZ)99547000000248449320181106j201705 ua 0engurmn|||||||||txtrdacontentcrdamediacrrdacarrierCompression-after-impact and bend fatigue results of glass/epoxy composites with compliant interlayer and needling inerlaminar enhancements /by Robert A Haynes, Steven E Boyd, Bradley D LawrenceAberdeen Proving Ground, MD :US Army Research Laboratory,May 2017.1 online resource (vi, 24 pages) color illustrationsARL-TR ;8022"May 2017."Includes bibliographical references (pages 20-22).Epoxy compoundsTestingComposite materialsTestingMaterialsFatigueTechnical reports.lcgftEpoxy compoundsTesting.Composite materialsTesting.MaterialsFatigue.Haynes Robert A.1420341Boyd Steven E.Lawrence Bradley D.U.S. Army Research Laboratory,GPOGPOGPOBOOK9910711555803321Compression-after-impact and bend fatigue results of glass3537863UNINA