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001 9910704876303321
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035   $a(OCoLC)860981117
035   $a(EXLCZ)995470000002444970
100   $a20131018d2013      ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aModel 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 /$fShantaram S. Pai, David S. Riha
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$d[2013]
215   $a1 online resource (9 pages) $cillustrations
225 1 $aNASA/TM 2013-217849
300   $aTitle from title screen (viewed Oct. 18, 2013).
300   $a"April 2013."
300   $aPrepared for the Turbo Expo 2012 sponsored by the American Society of Mechanical Engineers (ASME), Copenhagen, Denmark, June 11-15, 2012.
320   $aIncludes bibliographical references (page 9).
606   $aFlutter$2nasat
606   $aCracking (fracturing)$2nasat
606   $aPrediction analysis techniques$2nasat
606   $aFracture mechanics$2nasat
606   $aProbability theory$2nasat
606   $aProving$2nasat
606   $aFatigue life$2nasat
606   $aFatigue (materials)$2nasat
606   $aMathematical models$2nasat
615  7$aFlutter.
615  7$aCracking (fracturing)
615  7$aPrediction analysis techniques.
615  7$aFracture mechanics.
615  7$aProbability theory.
615  7$aProving.
615  7$aFatigue life.
615  7$aFatigue (materials)
615  7$aMathematical models.
700   $aPai$b Shantaram S.$01407131
702   $aRiha$b David S.
712 02$aUnited States.$bNational Aeronautics and Space Administration,
712 02$aNASA Glenn Research Center,
712 12$aASME Turbo Expo$f(2012 :$eCopenhagen, Denmark)
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910704876303321
996   $aModel 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$93494803
997   $aUNINA