01995nam 2200565I 450 991070587150332120170725075709.0(CKB)5470000002453700(OCoLC)994642614(EXLCZ)99547000000245370020170725j199806 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierA progressive damage methodology for residual strength predictions of notched composite panels /Timothy W. Coats and Charles E. HarrisHampton, Virginia :National Aeronautics and Space Administration, Langley Research Center,June 1998.1 online resource (43 pages) illustrationsNASA/TM ;1998-207646"June 1998.""Performing organization: NASA Langley Research Center"--Report documentation page.Includes bibliographical references (pages 22-24).Composite structuresnasatCrack propagationnasatEpoxy matrix compositesnasatFractographynasatFracture mechanicsnasatFracture strengthnasatLaminatesnasatLoads (forces)nasatResidual strengthnasatComposite structures.Crack propagation.Epoxy matrix composites.Fractography.Fracture mechanics.Fracture strength.Laminates.Loads (forces)Residual strength.Coats Timothy W.1397146Harris Charles E.1950-Langley Research Center,GPOGPOBOOK9910705871503321A progressive damage methodology for residual strength predictions of notched composite panels3458432UNINA