02052oam 2200529 450 991070702700332120160330150846.0(CKB)5470000002461220(OCoLC)755259956(EXLCZ)99547000000246122020111002j199706 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierFinite-element analysis of a Mach-8 flight test article using nonlinear contact elements /W. Lance Richards[Washington, D.C.] :National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program,June 1997.1 online resource (14 pages) illustrationsNASA technical memorandum ;4796Title from title screen (viewed March 30, 2016)."June 1997.""Performing organization: NASA Dryden Flight Research Center, Edwards, California"--Report documentation page.Includes bibliographical references (page 14).Finite element methodnasatHypersonic speednasatStructural designnasatHypersonic flightnasatNonlinearitynasatFinite element method.Hypersonic speed.Structural design.Hypersonic flight.Nonlinearity.Richards W. Lance1399318NASA Dryden Flight Research Center.United States.National Aeronautics and Space Administration.Scientific and Technical Information Program,United States.National Aeronautics and Space Administration,OCLCEOCLCEOCLCQOCLCOGPOBOOK9910707027003321Finite-element analysis of a Mach-8 flight test article using nonlinear contact elements3464298UNINA