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100   $a20110201d2010      ua             0
101 0 $aeng
135   $aurmn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 14$aThe effect of nondeterministic parameters on shock-associated noise prediction modeling$b[electronic resource] /$fMilo D. Dahl, Abbas Khavaran ; prepared for the 16th Aeroacoustics Conference cosponsored by the American Institute of Aeronautics and Astronautics and the Confederation of European Aerospace Societies, Stockholm, Sweden, June 7-9, 2010
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$d[2010]
215   $a1 online resource (24 pages) $cillustrations
225 1 $aNASA/TM ;$v2010-216801
300   $aTitle from title screen (viewed on Feb. 1, 2011).
300   $a"September 2010."
300   $a"AIAA-2010-3841."
320   $aIncludes bibliographical references (page 16).
606   $aAerodynamic noise$2nasat
606   $aSensitivity analysis$2nasat
606   $aNoise prediction$2nasat
606   $aSupersonic jet flow$2nasat
606   $aMathematical models$2nasat
606   $aProbability distribution functions$2nasat
615  7$aAerodynamic noise.
615  7$aSensitivity analysis.
615  7$aNoise prediction.
615  7$aSupersonic jet flow.
615  7$aMathematical models.
615  7$aProbability distribution functions.
700   $aDahl$b Milo D.$f1956-$01397975
701   $aKhavaran$b Abbas$f1953-$01397145
712 02$aNASA Glenn Research Center.
712 12$aAIAA/CEAS Aeroacoustics Conference$d(16th :$f2010 :$eStockholm, Sweden)
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910699957003321
996   $aThe effect of nondeterministic parameters on shock-associated noise prediction modeling$93510834
997   $aUNINA