LEADER 01886nam  2200505I  450 
001 9910702438303321
005 20150325141936.0
035   $a(CKB)5470000002427787
035   $a(OCoLC)905620862
035   $a(EXLCZ)995470000002427787
100   $a20150325j201404    ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aEffects of spent cooling and swirler angle on a 9-point swirl-venturi injector /$fZhuohui J. He [and four others]
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$dApril 2014.
215   $a1 online resource (7 pages) $ccolor illustrations
225 1 $aNASA/TM ;$v2014-218117
300   $aTitle from title screen (viewed on March 25, 2015).
300   $a"April 2014."
300   $a"Prepared for the 8th U.S. National Combustion Meeting sponsored by the Western State Section, Combustion Institute, Park City, Utah, May 19-22, 2013."
320   $aIncludes bibliographical references (page 7).
606   $aCombustion chambers$2nasat
606   $aInlet pressure$2nasat
606   $aInlet temperature$2nasat
606   $aFuel injection$2nasat
606   $aCombustion temperature$2nasat
606   $aNitrogen oxides$2nasat
615  7$aCombustion chambers.
615  7$aInlet pressure.
615  7$aInlet temperature.
615  7$aFuel injection.
615  7$aCombustion temperature.
615  7$aNitrogen oxides.
700   $aHe$b Zhuohui J.$01403836
712 02$aNASA Glenn Research Center,
712 02$aFundamental Aeronautics Program (U.S.),
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910702438303321
996   $aEffects of spent cooling and swirler angle on a 9-point swirl-venturi injector$93509488
997   $aUNINA