02244oam 2200553Ia 450 991070212140332120121031075307.0(CKB)5470000002424927(OCoLC)742768423(EXLCZ)99547000000242492720120810d2010 ua 0undurcn|||||||||txtrdacontentcrdamediacrrdacarrierComputational implementation of a thermodynamically based work potential model for progressive microdamage and transverse cracking in fiber-reinforced laminates[electronic resource] /Evan J. Pineda ... [and others]Cleveland, Ohio :National Aeronautics and Space Administration, Glenn Research Center,[2012]1 online resource (22 pages) color illustrationsNASA/TM ;2012-217243Title from title screen (viewed on Oct. 29, 2012)."Prepared for the 51th Structures, Structural Dynamics, and Materials Conference cosponsored by the AIAA, ASME, ASCE, AHS, and ASC Orlando, Florida, April 12-15, 2010.""May 2012.""AIAA-2010-2815."Includes bibliographical references (pages 21-22).Fiber compositesnasatLaminatesnasatContinuumsnasatFailure analysisnasatMicrocracksnasatPotential theorynasatTransverse loadsnasatFiber composites.Laminates.Continuums.Failure analysis.Microcracks.Potential theory.Transverse loads.Pineda Evan J1387412NASA Glenn Research Center.AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference(51st :2012 :Orlando, Fla.)EYMEYMGPOBOOK9910702121403321Computational implementation of a thermodynamically based work potential model for progressive microdamage and transverse cracking in fiber-reinforced laminates3530620UNINA