01891nam 2200553Ia 450 991070144970332120120308152323.0(CKB)5470000002418581(OCoLC)779542128(EXLCZ)99547000000241858120120308d2011 ua 0engurmn|||||||||txtrdacontentcrdamediacrrdacarrierDesign, optimization and evaluation of integrally stiffened Al 7050 panel with curved stiffeners[electronic resource] /Wesley C.H. Slemp ... [and others]Hampton, Va. :National Aeronautics and Space Administration, Langley Research Center,[2011]1 online resource (39 pages) illustrations (some color)NASA/TP ;2011-217178Title from title screen (viewed on Mar. 8, 2012)."September 2011."Includes bibliographical references (pages 22-23).BucklingnasatFinite element methodnasatDesign optimizationnasatLoad testsnasatElastic bucklingnasatWing panelsnasatFixturesnasatDeflectionnasatLoads (forces)nasatBuckling.Finite element method.Design optimization.Load tests.Elastic buckling.Wing panels.Fixtures.Deflection.Loads (forces)Slemp Wesley C. H1407850Langley Research Center.GPOGPOBOOK9910701449703321Design, optimization and evaluation of integrally stiffened Al 7050 panel with curved stiffeners3490282UNINA