01737nam 2200517Ia 450 991069716450332120230902161857.0(CKB)5470000002385266(OCoLC)696008010(EXLCZ)99547000000238526620110110d2006 ua 0engurmn|||||||||txtrdacontentcrdamediacrrdacarrierA thermodynamically consistent damage model for advanced composites[electronic resource] /Pere Maimí ... [and others]Hampton, Va. :National Aeronautics and Space Administration, Langley Research Center,[2006]1 online resource (42 pages) illustrationsNASA/TM- ;2006-214282Title from title screen (viewed on Jan. 10, 2011)."March 2006."Includes bibliographical references (pages 34-37).NASA technical memorandum ;214282.Composite materialsnasatDamagenasatContinuum modelingnasatFiber compositesnasatCrack closurenasatDegradationnasatLoads (forces)nasatComposite materials.Damage.Continuum modeling.Fiber composites.Crack closure.Degradation.Loads (forces)Maimí Pere1415407Langley Research Center.GPOGPOBOOK9910697164503321A thermodynamically consistent damage model for advanced composites3517339UNINA