00754nam a2200229 i 450099100376456970753620020506104515.0000908s1960 it ||| | ita b10552297-39ule_instEXGIL126605ExLBiblioteca Interfacoltà ita853.91Gotta, Salvator258084Orgasmo /Salvator GottaMilano :Mondadori,1960248 p. ;20 cm..b1055229702-04-1427-06-02991003764569707536LE002 It. XIX D 1312002000653284le002-E0.00-l- 00000.i1063449627-06-02Orgasmo215841UNISALENTOle00201-01-00ma -itait 0102126nam 2200517Ia 450 991069995700332120110209163334.0(CKB)5470000002406386(OCoLC)699819497(EXLCZ)99547000000240638620110201d2010 ua 0engurmn|||||||||txtrdacontentcrdamediacrrdacarrierThe effect of nondeterministic parameters on shock-associated noise prediction modeling[electronic resource] /Milo 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, 2010Cleveland, Ohio :National Aeronautics and Space Administration, Glenn Research Center,[2010]1 online resource (24 pages) illustrationsNASA/TM ;2010-216801Title from title screen (viewed on Feb. 1, 2011)."September 2010.""AIAA-2010-3841."Includes bibliographical references (page 16).Aerodynamic noisenasatSensitivity analysisnasatNoise predictionnasatSupersonic jet flownasatMathematical modelsnasatProbability distribution functionsnasatAerodynamic noise.Sensitivity analysis.Noise prediction.Supersonic jet flow.Mathematical models.Probability distribution functions.Dahl Milo D.1956-1397975Khavaran Abbas1953-1397145NASA Glenn Research Center.AIAA/CEAS Aeroacoustics Conference(16th :2010 :Stockholm, Sweden)GPOGPOBOOK9910699957003321The effect of nondeterministic parameters on shock-associated noise prediction modeling3510834UNINA