LEADER 02446nam  2200685   450 
001 9910705817403321
005 20170809125659.0
035   $a(CKB)5470000002454247
035   $a(OCoLC)1000155042
035   $a(EXLCZ)995470000002454247
100   $a20170809j199811    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aBenefits of swept and leaned stators for fan noise reduction /$fRichard P. Woodward [and three others]
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Lewis Research Center,$dNovember 1998.
215   $a1 online resource (30 pages) $cillustrations
225 1 $aNASA/TM ;$v1998-208661
300   $a"November 1998."
300   $a"Prepared for the 37th Aerospace Sciences Meeting and Exhibit sponsored by the American Institute of Aeronautics and Astronautics, Reno, Nevada, January 11-14, 1999."
300   $a"Performing organization: National Aeronautics and Space Administration, Lewis Research Center"--Report documentation page.
300 1 $aWoodward, Richard P.,$eauthor.
320   $aIncludes bibliographical references (page 8).
606   $aAcoustic properties$2nasat
606   $aAerodynamic characteristics$2nasat
606   $aAerodynamic noise$2nasat
606   $aNoise reduction$2nasat
606   $aStators$2nasat
606   $aVanes$2nasat
606   $aWind tunnel tests$2nasat
606   $aStator blades$2nasat
606   $aEngine noise$2nasat
606   $aJet aircraft noise$2nasat
606   $aSweep effect$2nasat
606   $aEffective perceived noise levels$2nasat
606   $aFans$2nasat
615  7$aAcoustic properties.
615  7$aAerodynamic characteristics.
615  7$aAerodynamic noise.
615  7$aNoise reduction.
615  7$aStators.
615  7$aVanes.
615  7$aWind tunnel tests.
615  7$aStator blades.
615  7$aEngine noise.
615  7$aJet aircraft noise.
615  7$aSweep effect.
615  7$aEffective perceived noise levels.
615  7$aFans.
700   $aWoodward$b Richard P.$01411998
712 02$aLewis Research Center,
801  0$bGPO
801  1$bGPO
801  2$bGPO
906   $aBOOK
912   $a9910705817403321
996   $aBenefits of swept and leaned stators for fan noise reduction$93504395
997   $aUNINA