01968nam 2200493I 450 991070415870332120160106095059.0(CKB)5470000002438077(OCoLC)933758756(EXLCZ)99547000000243807720160106j201508 ua 0engurcn|||||||||txtrdacontentcrdamediacrrdacarrierA numerical study on the effect of facesheet-core disbonds on the buckling load of curved honeycomb sandwich panels /Evan J. Pineda [and three others]Cleveland, Ohio :National Aeronautics and Space Administration, Glenn Research Center,August 2015.1 online resource (18 pages) color illustrationsNASA/TM ;2015-218861Title from title screen (viewed on Jan. 6, 2016)."August 2015.""Prepared for the 30th Annual Technical Conference sponsored by the American Society for Composites, East Lansing, Michigan, September 28-30, 2015.""Paper no. 1713."Includes bibliographical references (pages 16-18).Spacecraft shieldingnasatCurved panelsnasatHoneycomb coresnasatDebonding (materials)nasatHeavy lift launch vehiclesnasatSpacecraft shielding.Curved panels.Honeycomb cores.Debonding (materials)Heavy lift launch vehicles.Pineda Evan J.1387412NASA Glenn Research Center,United States.National Aeronautics and Space Administration,GPOGPOBOOK9910704158703321A numerical study on the effect of facesheet-core disbonds on the buckling load of curved honeycomb sandwich panels3459422UNINA