01613nam 2200469Ia 450 991069980120332120110624143508.0(CKB)5470000002404929(OCoLC)700073286(EXLCZ)99547000000240492920110202d2010 ua 0engurmn|||||||||txtrdacontentcrdamediacrrdacarrierDevelopment of a benchmark example for delamination fatigue growth prediction[electronic resource] /Ronald KruegerHampton, Va. :National Aeronautics and Space Administration, Langley Research Center,[2010]1 online resource (46 pages) illustrationsNASA/CR-2010-216723Title from title screen (viewed on Feb. 2, 2011)."July 2010.""NIA Report No. 2010-04."Includes bibliographical references (page 207).DelaminatingnasatComposite materialsnasatFinite element methodnasatCyclic loadsnasatMathematical modelsnasatDelaminating.Composite materials.Finite element method.Cyclic loads.Mathematical models.Krueger Ronald1395935Langley Research Center.GPOGPOBOOK9910699801203321Development of a benchmark example for delamination fatigue growth prediction3496602UNINA