01771nam 2200505I 450 991070378430332120150501110201.0(CKB)5470000002433875(OCoLC)908252076(EXLCZ)99547000000243387520150501j198708 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierPostbuckling delamination of a stiffened composite panel using finite element methods /S. Natsiavas, C.D. Babcock and W.G. KnaussPasadena, California :California Institute of Technology,August, 1987.1 online resource (9 pages, 10 unnumbered pages) illustrationsNASA/CR ;182803Title from title screen (viewed May 1, 2015)."August, 1987.""GALCIT SM report 87-19."Includes bibliographical references (pages 8-9).BucklingnasatDelaminatingnasatFinite element methodnasatCompression loadsnasatPlate theorynasatBuckling.Delaminating.Finite element method.Compression loads.Plate theory.Natsiavas S.1423118Babcock Charles D.Knauss Wolfgang GustavCalifornia Institute of Technology,United States.National Aeronautics and Space Administration,GPOGPOBOOK9910703784303321Postbuckling delamination of a stiffened composite panel using finite element methods3549549UNINA