01769oam 2200517I 450 991071408880332120201211102929.0(CKB)5470000002506781(OCoLC)761231417(EXLCZ)99547000000250678120111115j196903 ua 0engur|||||||||||txtrdacontentcrdamediacrrdacarrierMechanical behavior of boron-epoxy and glass-epoxy filament-wound cylinders under various loads /by Harvey W. Herring, Robert M. Baucom, and Richard A. PrideWashington, D.C. :National Aeronautics and Space Administration,March 1969.1 online resource (65 pages) illustrationsNASA technical note ;NASA TN D-5050"March 1969."Includes bibliographical references (pages 20-21).CylindersTestingFibrous compositesTestingCylindersTestingfastFibrous compositesTestingfastCylindersTesting.Fibrous compositesTesting.CylindersTesting.Fibrous compositesTesting.Herring Harvey W.1419398Baucom Robert M.Pride Richard A.United States.National Aeronautics and Space Administration,OCLCEOCLCEOCLCQOCLCOOCLCFOCLCQCOPGPOBOOK9910714088803321Mechanical behavior of boron-epoxy and glass-epoxy filament-wound cylinders under various loads3533702UNINA