LEADER 01819nam  2200493   450 
001 9910702436203321
005 20140709141431.0
035   $a(CKB)5470000002427808
035   $a(OCoLC)883242288
035   $a(EXLCZ)995470000002427808
100   $a20140709j201311    ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aEffect of two advanced noise reduction technologies on the aerodynamic performance of an ultra high bypass ratio fan /$fChristopher E. Hughes, John A. Gazzaniga
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Langley Research Center,$dNovember 2013.
215   $a1 online resource (22 pages) $ccolor illustrations
225 1 $aNASA/TM ;$v2013-216073
300   $aTitle from title screen (viewed July 9, 2014).
300   $a"November 2013."
320   $aIncludes bibliographical references (pages 5-6).
606   $aAircraft performance$2nasat
606   $aBypass ratio$2nasat
606   $aFan blades$2nasat
606   $aFixed wings$2nasat
606   $aLow speed wind tunnels$2nasat
606   $aNoise reduction$2nasat
615  7$aAircraft performance.
615  7$aBypass ratio.
615  7$aFan blades.
615  7$aFixed wings.
615  7$aLow speed wind tunnels.
615  7$aNoise reduction.
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   $a9910702436203321
996   $aEffect of two advanced noise reduction technologies on the aerodynamic performance of an ultra high bypass ratio fan$93473454
997   $aUNINA