01601nam 2200445I 450 991070651020332120171215151520.0(CKB)5470000002457350(OCoLC)1015382343(EXLCZ)99547000000245735020171215j201709 ua 0engurmn|||||||||txtrdacontentcrdamediacrrdacarrierGuidelines for VCCT-based interlaminar fatigue and progressive failure finite element analysis /Lyle R. Deobald [and twelve others]Hampton, Virginia :National Aeronautics and Space Administration, Langley Research Center,September 2017.1 online resource (32 unnumbered pages) color illustrationsNASA/TM ;2017-219663"September 2017."Includes bibliographical references (pages 30-31).Aerospace industrynasatFailure analysisnasatFinite element methodnasatStructural analysisnasatComposite materialsnasatAerospace industry.Failure analysis.Finite element method.Structural analysis.Composite materials.Deobald Lyle R.1389975Langley Research Center,GPOGPOBOOK9910706510203321Guidelines for VCCT-based interlaminar fatigue and progressive failure finite element analysis3442177UNINA