02350oam 2200601I 450 991070439910332120170816114731.0(CKB)5470000002439689(OCoLC)778057800(EXLCZ)99547000000243968920120223j199611 ua 0engurbn||||a|a||txtrdacontentcrdamediacrrdacarrierProgressive Damage Analysis of Laminated Composite (PDALC) a computational model implemented in the NASA COMET finite element code /David C. Lo [and three others]Hampton, Virginia :National Aeronautics and Space Administration, Langley Research Center,November 1996.1 online resource (41 pages) illustrationsNASA technical memorandum ;4724Title from title screen (viewed on Feb. 23, 2016)."November 1996.""Performing organization: NASA Langley Research Center, Hampton, VA"--Report documentation page.Includes bibliographical references (page 32).Progressive Damage Analysis of Laminated Composite Laminated materialsCrackingMathematical modelsComposite materialsCrackingMathematical modelsFinite element methodData processingResidual strengthnasatStructural analysisnasatMatrix materialsnasatCracking (fracturing)nasatDamage assessmentnasatLaminated materialsCrackingMathematical models.Composite materialsCrackingMathematical models.Finite element methodData processing.Residual strength.Structural analysis.Matrix materials.Cracking (fracturing)Damage assessment.Lo David C.1419697Langley Research Center,United States.National Aeronautics and Space Administration,OCLCEOCLCEOCLCQOCLCOGPOBOOK9910704399103321Progressive Damage Analysis of Laminated Composite (PDALC)3535091UNINA