02318nam 2200577Ia 450 991069991840332120110421144329.0(CKB)5470000002406776(OCoLC)713885807(EXLCZ)99547000000240677620110421d2010 ua 0engurmn|||||||||txtrdacontentcrdamediacrrdacarrierOptical characterization of a multipoint lean direct injector for gas turbine combustors[electronic resource] velocity and fuel drop size measurements /Christopher M. Heath ... [and others] ; prepared for the Turbo Expo 2010 sponsored by the American Society of Mechanical Engineers (ASME), Glasgow, Scotland, United Kingdom, June 14-18, 2010Cleveland, Ohio :National Aeronautics and Space Administration, Glenn Research Center,[2010]1 online resource (13 pages) illustrations, colorNASA/TM ;2010-216365Title from title screen (viewed on April 21, 2011)."October 2010."Includes bibliographical references (page 13).Optical characterization of a multipoint lean direct injector for gas turbine combustors Fuel injectionnasatGas turbinesnasatFlight conditionsnasatComputational fluid dynamicsnasatCombustion chambersnasatAircraft enginesnasatFlame temperaturenasatInlet temperaturenasatSupersonic flightnasatFuel injection.Gas turbines.Flight conditions.Computational fluid dynamics.Combustion chambers.Aircraft engines.Flame temperature.Inlet temperature.Supersonic flight.Heath Christopher M1395901NASA Glenn Research Center.ASME Turbo Expo(2010 :Glasgow, Scotland)GPOGPOBOOK9910699918403321Optical characterization of a multipoint lean direct injector for gas turbine combustors3455151UNINA