01733nam 2200493I 450 991070462920332120130705144259.0(CKB)5470000002443425(OCoLC)851803234(EXLCZ)99547000000244342520130705d2013 ua 0engurmn|||||||||txtrdacontentcrdamediacrrdacarrierNormalization of impact energy by laminate thickness for compression after impact testing /A.T. Nettles and S.M. HromisinHuntsville, Alabama :National Aeronautics and Space Administration, Marshall Space Flight Center,2013.1 online resource (ix, 37 pages) illustrations (some color)NASA/TP ;2013-217481Title from title screen (viewed on July 5, 2013)."April 2013."Includes bibliographical references (pages 35-37).LaminatesnasatThicknessnasatImpact strengthnasatCompression loadsnasatMechanical propertiesnasatImpact tolerancesnasatLaminates.Thickness.Impact strength.Compression loads.Mechanical properties.Impact tolerances.Nettles A. T(Alan T.),1389578Hromisin S. M.George C. Marshall Space Flight Center,GPOGPOBOOK9910704629203321Normalization of impact energy by laminate thickness for compression after impact testing3491715UNINA