LEADER 01933nam 2200469 450 001 9910702487903321 005 20130212090504.0 035 $a(CKB)5470000002427286 035 $a(OCoLC)827269453 035 $a(EXLCZ)995470000002427286 100 $a20130212d2012 ua 0 101 0 $aeng 135 $aurmn||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aPredicting the inflow distortion tone noise of the NASA Glenn Advanced Noise Control Fan with a combined quadrupole-dipole model /$fL. Danielle Koch 210 1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$d2012. 215 $a1 online resource (16 pages) $cillustrations (some color) 225 1 $aNASA/TM ;$v2012-217673 300 $aTitle from title screen (viewed on Jan. 14, 2013). 300 $a"September 2012." 300 $a"Prepared for the 18th Aeroacoustics Conference cosponsored by the American Institute of Aeronautics and Astronautics and Confederation of European Aerospace Societies, Colorado Springs, Colorado, June 4-6, 2012." 300 $a"AIAA-2012-2196." 320 $aIncludes bibliographical references (page 7). 606 $aAerodynamic noise$2nasat 606 $aNoise prediction$2nasat 606 $aPredictions$2nasat 606 $aAsymmetry$2nasat 615 7$aAerodynamic noise. 615 7$aNoise prediction. 615 7$aPredictions. 615 7$aAsymmetry. 700 $aKoch$b L. Danielle$01390396 712 02$aNASA Glenn Research Center, 712 12$aAIAA/CEAS Aeroacoustics Conference$d(18th :$f2012 :$eColorado Springs, Colo.) 801 0$bGPO 801 1$bGPO 906 $aBOOK 912 $a9910702487903321 996 $aPredicting the inflow distortion tone noise of the NASA Glenn Advanced Noise Control Fan with a combined quadrupole-dipole model$93443021 997 $aUNINA