01753nam 2200493 450 991070481630332120140212082156.0(CKB)5470000002445576(OCoLC)870332862(EXLCZ)99547000000244557620140212d2013 ua 0engurcn|||||||||txtrdacontentcrdamediacrrdacarrierAn Approximate solution and master curves for buckling of symmetrically laminated composite cylinders /Michael P. NemethHampton, Virginia :National Aeronautics and Space Administration, Langley Research Center,2013.1 online resource (60 pages) color illustrationsNASA/TM ;2013-217999Title from title screen (viewed on Feb. 12, 2014)."May 2013."Includes bibliographical references (page 19).AnisotropynasatAxial compression loadsnasatCylindrical shellsnasatInhomogeneitynasatLaminatesnasatSandwich structuresnasatAnisotropy.Axial compression loads.Cylindrical shells.Inhomogeneity.Laminates.Sandwich structures.Nemeth Michael P.1391721Langley Research Center,United States.National Aeronautics and Space Administration,GPOGPOBOOK9910704816303321An Approximate solution and master curves for buckling of symmetrically laminated composite cylinders3514065UNINA