01908nam 2200505Ia 450 991069931510332120230902161818.0(CKB)5470000002402769(OCoLC)724603603(EXLCZ)99547000000240276920110517d2006 ua 0engurcn|||||||||txtrdacontentcrdamediacrrdacarrierInfluence of finite element software on energy release rates computed using the virtual crack closure technique[electronic resource] /Ronald Krueger, Dirk GoetzeHampton, Va. :National Aeronautics and Space Administration, Langley Research Center,[2006]1 online resource (49 pages) illustrations (some color)NAS/CR ;2006-214523Title from title screen (viewed on May 16, 2011)."October 2006.""Prepared for Langley Research Center.""National Institute of Aerospace.""NIA Report no. 2006-06."Includes bibliographical references (pages 15-17).NASA contractor report ;NAS/CR-2006-214523.Finite element methodnasatStrain energy release ratenasatCrack closurenasatDelaminatingnasatFinite element method.Strain energy release rate.Crack closure.Delaminating.Krueger Ronald1395935Goetze Dirk1395936Langley Research Center.National Institute of Aerospace.GPOGPOBOOK9910699315103321Influence of finite element software on energy release rates computed using the virtual crack closure technique3455213UNINA