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001 9910700138803321
005 20140129154302.0
035   $a(CKB)5470000002407580
035   $a(OCoLC)707645081
035   $a(EXLCZ)995470000002407580
100   $a20110317g20102011  ua             0
101 0 $aeng
135   $aurmn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aResults of an advanced fan stage operating over a wide range of speed and bypass ratio /$fKenneth L. Suder [and five others]
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$d[2010]-[2011]
215   $a1 online resource (2 volumes) $ccolor illustrations
225 1 $aNASA/TM ;$v2010-216769, 2011-216769
300   $aTitle from title screen (viewed on Jan. 29, 2014).
300   $a"Prepared for the Turbo Expo 2010 sponsored by the American Society of Mechanical Engineers (ASME), Glasgow, Scotland, United Kingdom, June 14-18, 2010."
320   $aIncludes bibliographical references.
327   $apt. 1. Fan stage design and experimental results -- pt 2. Comparison of CFD and experimental results.
606   $aAerodynamic stalling$2nasat
606   $aBypass ratio$2nasat
606   $aComputational fluid dynamics$2nasat
606   $aPropulsion system configurations$2nasat
606   $aTransonic compressors$2nasat
606   $aTurbofans$2nasat
606   $aSupersonic speed$2nasat
606   $aComputerized simulation$2nasat
615  7$aAerodynamic stalling.
615  7$aBypass ratio.
615  7$aComputational fluid dynamics.
615  7$aPropulsion system configurations.
615  7$aTransonic compressors.
615  7$aTurbofans.
615  7$aSupersonic speed.
615  7$aComputerized simulation.
700   $aSuder$b Kenneth L$g(Kenneth Lee)$01391483
712 02$aFundamental Aeronautics Program (U.S.),
712 02$aNASA Glenn Research Center,
712 12$aASME Turbo Expo$f(2010 :$eGlasgow, Scotland)
801  0$bGPO
801  1$bGPO
801  2$bGPO
801  2$bOCLCQ
801  2$bGPO
906   $aBOOK
912   $a9910700138803321
996   $aResults of an advanced fan stage operating over a wide range of speed and bypass ratio$93445297
997   $aUNINA