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100   $a20110420d2010      ua             0
101 0 $aeng
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181   $ctxt$2rdacontent
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200 10$aPredicted and measured modal sound power levels for a fan ingesting distorted inflow$b[electronic resource] /$fL. Danielle Koch ; 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 (15 pages) $cillustrations, color
225 1 $aNASA/TM ;$v2010-216782
300   $aTitle from title screen (viewed on April 20, 2011).
300   $a"August 2010."
300   $a"AIAA-2010-223128."
320   $aIncludes bibliographical references (page 5).
606   $aFan blades$2nasat
606   $aAerodynamic noise$2nasat
606   $aSound pressure$2nasat
606   $aCylindrical bodies$2nasat
606   $aNoise intensity$2nasat
606   $aUpstream$2nasat
615  7$aFan blades.
615  7$aAerodynamic noise.
615  7$aSound pressure.
615  7$aCylindrical bodies.
615  7$aNoise intensity.
615  7$aUpstream.
700   $aKoch$b L. Danielle$01390396
712 02$aNASA Glenn Research Center.
712 12$aAIAA/CEAS Aeroacoustics Conference$d(16th :$f2010 :$eStockholm, Sweden)
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