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100   $a20120830d2012      ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aFull-scale turbofan-engine turbine-transfer function determination using three internal sensors$b[electronic resource] /$fLennart S. Hultgren ; prepared for the 17th Aeroacoustics Conference sponsored by the American Institute of Aeronautics and Astronautics and the Confederation of European Aerospace Societies, Portland, Oregon, June 5-8, 2011
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$d[2012]
215   $a1 online resource (13 pages) $ccolor illustrations
225 1 $aNASA/TM ;$v2012-217252
300   $aTitle from title screen (viewed on Aug. 30, 2012).
300   $a"February 2012."
300   $a"AIAA-2011-2912."
320   $aIncludes bibliographical references (pages 12-13).
606   $aTurbofan engines$2nasat
606   $aTransfer functions$2nasat
606   $aEngine tests$2nasat
606   $aNoise generators$2nasat
606   $aStatic tests$2nasat
606   $aNoise prediction$2nasat
615  7$aTurbofan engines.
615  7$aTransfer functions.
615  7$aEngine tests.
615  7$aNoise generators.
615  7$aStatic tests.
615  7$aNoise prediction.
700   $aHultgren$b Lennart S$g(Lennart Sven)$01386308
712 02$aNASA Glenn Research Center.
712 12$aAIAA/CEAS Aeroacoustics Conference$d(17th :$f2011 :$ePortland, Or.)
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910701910703321
996   $aFull-scale turbofan-engine turbine-transfer function determination using three internal sensors$93480728
997   $aUNINA