LEADER 02020nam  2200553   450 
001 9910702436703321
005 20140709114120.0
035   $a(CKB)5470000002427803
035   $a(OCoLC)883215359
035   $a(EXLCZ)995470000002427803
100   $a20140709j201312    ua             0
101 0 $aeng
135   $aurmn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 14$aThe effect of bypass nozzle exit area on fan aerodynamic performance and noise in a model turbofan simulator /$fChristopher E. Hughes [and three others]
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$dDecember 2013.
215   $a1 online resource (35 pages) $cillustrations (some color)
225 1 $aNASA/TM ;$v2013-214029
300   $aTitle from title screen (viewed July 9, 2014).
300   $a"December 2013."
300   $a"GT2005-68573."
320   $aIncludes bibliographical references (page 13).
606   $aAeroacoustics$2nasat
606   $aAerodynamic characteristics$2nasat
606   $aAerodynamic noise$2nasat
606   $aAircraft noise$2nasat
606   $aFan blades$2nasat
606   $aFar fields$2nasat
606   $aLaser doppler velocimeters$2nasat
606   $aLow speed wind tunnels$2nasat
615  7$aAeroacoustics.
615  7$aAerodynamic characteristics.
615  7$aAerodynamic noise.
615  7$aAircraft noise.
615  7$aFan blades.
615  7$aFar fields.
615  7$aLaser doppler velocimeters.
615  7$aLow speed wind tunnels.
700   $aHughes$b Christopher E.$01402594
712 02$aNASA Glenn Research Center,
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910702436703321
996   $aThe effect of bypass nozzle exit area on fan aerodynamic performance and noise in a model turbofan simulator$93489728
997   $aUNINA