01770nam 2200505Ia 450 991070221040332120121113143249.0(CKB)5470000002426049(OCoLC)817725601(EXLCZ)99547000000242604920121113d2012 ua 0engurmn|||||||||txtrdacontentcrdamediacrrdacarrierDesign, optimization, and evaluation of A1-2139 compression panel with integral T-stiffeners[electronic resource] /Sameer B. Mulani ... [and others]Hampton, Va. :National Aeronautics and Space Administration, Langley Research Center,[2012]1 online resource (x, 33 pages) illustrations (some color)NASA/TP ;2012-217584Title from title screen (viewed on Nov. 13, 2012)."June 2012."Includes bibliographical references (pages 20-22).Design optimizationnasatFinite element methodnasatPhotogrammetrynasatAluminum alloysnasatDigital systemsnasatDisplacementnasatBucklingnasatDesign optimization.Finite element method.Photogrammetry.Aluminum alloys.Digital systems.Displacement.Buckling.Mulani Sameer B1417407Langley Research Center.GPOGPOBOOK9910702210403321Design, optimization, and evaluation of A1-2139 compression panel with integral T-stiffeners3525673UNINA