01924oam 2200493 450 991070438090332120160302141918.0(CKB)5470000002439873(OCoLC)777248062(EXLCZ)99547000000243987320120213j199612 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierThermal and mechanical buckling analysis of hypersonic aircraft hat-stiffened panels with varying face sheet geometry and fiber orientation /William L. Ko[Washington, D.C.] :National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program,December 1996.1 online resource (v, 30 pages) illustrationsNASA technical memorandum ;4770Title from title screen (viewed March 2, 2016)."December 1996."Includes bibliographical references (page 15).Aircraft structuresnasatThermal bucklingnasatMechanical propertiesnasatFinite element methodnasatHypersonic aircraftnasatAircraft structures.Thermal buckling.Mechanical properties.Finite element method.Hypersonic aircraft.Ko William L.1388928United States.National Aeronautics and Space Administration.Scientific and Technical Information Program,OCLCEOCLCEOCLCQOCLCOGPOBOOK9910704380903321Thermal and mechanical buckling analysis of hypersonic aircraft hat-stiffened panels with varying face sheet geometry and fiber orientation3466184UNINA