01886nam 2200505I 450 991070243830332120150325141936.0(CKB)5470000002427787(OCoLC)905620862(EXLCZ)99547000000242778720150325j201404 ua 0engurcn|||||||||txtrdacontentcrdamediacrrdacarrierEffects of spent cooling and swirler angle on a 9-point swirl-venturi injector /Zhuohui J. He [and four others]Cleveland, Ohio :National Aeronautics and Space Administration, Glenn Research Center,April 2014.1 online resource (7 pages) color illustrationsNASA/TM ;2014-218117Title from title screen (viewed on March 25, 2015)."April 2014.""Prepared for the 8th U.S. National Combustion Meeting sponsored by the Western State Section, Combustion Institute, Park City, Utah, May 19-22, 2013."Includes bibliographical references (page 7).Combustion chambersnasatInlet pressurenasatInlet temperaturenasatFuel injectionnasatCombustion temperaturenasatNitrogen oxidesnasatCombustion chambers.Inlet pressure.Inlet temperature.Fuel injection.Combustion temperature.Nitrogen oxides.He Zhuohui J.1403836NASA Glenn Research Center,Fundamental Aeronautics Program (U.S.),GPOGPOBOOK9910702438303321Effects of spent cooling and swirler angle on a 9-point swirl-venturi injector3509488UNINA