02282nam 2200541 a 450 991070096440332120111228112311.0(CKB)5470000002413382(OCoLC)769651307(EXLCZ)99547000000241338220111228d2011 ua 0engurcn|||||||||txtrdacontentcrdamediacrrdacarrierSeparating direct and indirect turbofan engine combustion noise while estimating post-combustion (post-flame) residence time using the correlation function[electronic resource] /Jeffrey Hilton MilesCleveland, Ohio :National Aeronautics and Space Administration, Glenn Research Center,[2011]1 online resource (21 pages) illustrations (chiefly color)NASA/TM ;2011-216248Title from title screen (viewed on Dec. 28, 2011)."Prepared for the 48th Aerospace Sciences Meeting sponsored by the American Institute of Aeronautics and Astronautics, Orlando, Florida, January 4-7, 2010.""May 2011.""AIAA-2010-0019."Includes bibliographical references (page 21).Separating direct and indirect turbofan engine combustion noise while estimating post-combustion AcousticsnasatCombustion chambersnasatTurbofan enginesnasatCross correlationnasatEngine testsnasatTime lagnasatAcoustics.Combustion chambers.Turbofan engines.Cross correlation.Engine tests.Time lag.Miles Jeffrey H(Jeffrey Hilton)1401187American Institute of Aeronautics and Astronautics.NASA Glenn Research Center.AIAA Aerospace Sciences Meeting(48th :2010 :Orlando, Fla.)GPOGPOBOOK9910700964403321Separating direct and indirect turbofan engine combustion noise while estimating post-combustion (post-flame) residence time using the correlation function3547511UNINA