02411nam 2200601I 450 991070487630332120131018083139.0(CKB)5470000002444970(OCoLC)860981117(EXLCZ)99547000000244497020131018d2013 ua 0engurcn|||||||||txtrdacontentcrdamediacrrdacarrierModel verification and validation concepts for a probabilistic fracture assessment model to predict cracking of knife edge seals in the space shuttle main engine high pressure oxidizer /Shantaram S. Pai, David S. RihaCleveland, Ohio :National Aeronautics and Space Administration, Glenn Research Center,[2013]1 online resource (9 pages) illustrationsNASA/TM 2013-217849Title from title screen (viewed Oct. 18, 2013)."April 2013."Prepared for the Turbo Expo 2012 sponsored by the American Society of Mechanical Engineers (ASME), Copenhagen, Denmark, June 11-15, 2012.Includes bibliographical references (page 9).FlutternasatCracking (fracturing)nasatPrediction analysis techniquesnasatFracture mechanicsnasatProbability theorynasatProvingnasatFatigue lifenasatFatigue (materials)nasatMathematical modelsnasatFlutter.Cracking (fracturing)Prediction analysis techniques.Fracture mechanics.Probability theory.Proving.Fatigue life.Fatigue (materials)Mathematical models.Pai Shantaram S.1407131Riha David S.United States.National Aeronautics and Space Administration,NASA Glenn Research Center,ASME Turbo Expo(2012 :Copenhagen, Denmark)GPOGPOBOOK9910704876303321Model verification and validation concepts for a probabilistic fracture assessment model to predict cracking of knife edge seals in the space shuttle main engine high pressure oxidizer3494803UNINA