01697nam 2200445I 450 991070620480332120171106132245.0(CKB)5470000002456394(OCoLC)1009737603(EXLCZ)99547000000245639420171106j200012 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierIn-plane and interlaminar shear strength of a unidirectional Hi-Nicalon fiber-reinforced celsian matrix composite /Ö. Ünal and N.P. BansalCleveland, Ohio :National Aeronautics and Space Administration, Glenn Research Center,December 2000.1 online resource (21 pages) illustrationsNASA/TM ;2000-210608"December 2000.""Performing organization: National Aeronautics and Space Administration, John H. Glenn Research Center at Lewis Field"--Report documentation page.Includes bibliographical references (pages 11-12).Fiber compositesnasatShear stressnasatStress analysisnasatSilicon carbidesnasatFiber composites.Shear stress.Stress analysis.Silicon carbides.Ünal Ö.1412156Bansal Narottam P.NASA Glenn Research Center,GPOGPOBOOK9910706204803321In-plane and interlaminar shear strength of a unidirectional Hi-Nicalon fiber-reinforced celsian matrix composite3504942UNINA