01967nam 2200469 450 991070570500332120170711091617.0(CKB)5470000002453362(OCoLC)993435119(EXLCZ)99547000000245336220170711j201703 ua 0engurcn|||||||||txtrdacontentcrdamediacrrdacarrierBuckling test results and preliminary test and analysis correlation from the 8-foot-diameter orthogrid-stiffened cylinder test article TA02: test dates: 3-6 February 2009 /Mark W. Hilburger [and three others]Hampton, Virginia :National Aeronautics and Space Administration, Langley Research Center,March 2017.1 online resource (x, 91 pages) color illustrationsNASA/TP ;2017-219587"March 2017.""Performing organization: NASA Langley Research Center"--Report documentation page.Includes bibliographical references (page 80).Buckling test results and preliminary test and analysis correlation from the 8-foot-diameter orthogrid-stiffened cylinder test article TA02BucklingnasatCompression loadsnasatCylindrical shellsnasatLaunch vehiclesnasatAluminum alloysnasatBuckling.Compression loads.Cylindrical shells.Launch vehicles.Aluminum alloys.Hilburger Mark W(Mark William),1395062Langley Research Center,GPOGPOBOOK9910705705003321Buckling test results and preliminary test and analysis correlation from the 8-foot-diameter orthogrid-stiffened cylinder test article TA02: test dates: 3-6 February 20093453051UNINA