LEADER 01973nam  2200505   450 
001 9910702435703321
005 20150325141619.0
035   $a(CKB)5470000002427813
035   $a(OCoLC)905620536
035   $a(EXLCZ)995470000002427813
100   $a20150325j201403    ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aComparison of computational aeroacoustics prediction of acoustic transmission through a 3D stator with experiment /$fRay Hixon [and three others]
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$dMarch 2014.
215   $a1 online resource (12 pages) $ccolor illustrations
225 1 $aNASA/TM ;$v2014-218113
300   $aTitle from title screen (viewed on March 25, 2015).
300   $a"March 2014."
300   $a"Prepared for the SciTech 2014 sponsored by the American Institute of Aeronautics and Astronautics, National Harbor, Maryland, January 13-17, 2014."
320   $aIncludes bibliographical references (pages 9-10).
606   $aComputational aeroacoustics$2nasat
606   $aAcoustic simulation$2nasat
606   $aAerodynamic noise$2nasat
606   $aTurbomachine blades$2nasat
606   $aNavier-Stokes equation$2nasat
606   $aEuler$2nasat
615  7$aComputational aeroacoustics.
615  7$aAcoustic simulation.
615  7$aAerodynamic noise.
615  7$aTurbomachine blades.
615  7$aNavier-Stokes equation.
615  7$aEuler.
700   $aHixon$b R$g(Ray),$01409652
712 02$aNASA Glenn Research Center,
712 02$aFundamental Aeronautics Program (U.S.),
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910702435703321
996   $aComparison of computational aeroacoustics prediction of acoustic transmission through a 3D stator with experiment$93527239
997   $aUNINA