02881oam 2200853 450 991070525120332120210820074229.0(CKB)5470000002448855(OCoLC)889078029(EXLCZ)99547000000244885520140825g20132014 ua 0engurcn|||||||||txtrdacontentcrdamediacrrdacarrierBuckling testing and analysis of honeycomb sandwich panel arc segments of a full-scale fairing barrel /David E. Myers, Evan J. Pineda [and four others]Cleveland, Ohio :National Aeronautics and Space Administration, Glenn Research Center,2013-2014.1 online resource (3 volumes) color illustrationsNASA/TM ;2013-217822NASA/TM ;2014-217822Includes bibliographical references.pt. 1. 8-ply in-autoclave facesheets -- pt. 2. 6-ply in-autoclave facesheets -- pt. 3. 8-ply out-of-autoclave facesheets.Fibrous compositesFinite element methodHoneycomb structuresFibrous compositesfastFinite element methodfastHoneycomb structuresfastAres 5 cargo launch vehiclenasatEpoxy matrix compositesnasatFiber compositesnasatFinite element methodnasatHoneycomb structuresnasatRobustness (mathematics)nasatSandwich structuresnasatTechnical reports.fastEbook.Technical reports.lcgftFibrous composites.Finite element method.Honeycomb structures.Fibrous composites.Finite element method.Honeycomb structures.Ares 5 cargo launch vehicle.Epoxy matrix composites.Fiber composites.Finite element method.Honeycomb structures.Robustness (mathematics)Sandwich structures.Myers David E(Engineer),328638Pineda Evan J.NASA Glenn Research Center,United States.National Aeronautics and Space Administration,GPOGPOGPODIBIBLWAOCLCOOCLCFINTOCLCQOCLCOXFFOCLOCLCQGPOBOOK9910705251203321Buckling testing and analysis of honeycomb sandwich panel arc segments of a full-scale fairing barrel3539258UNINA