01966nam 2200493I 450 991070378230332120150526162452.0(CKB)5470000002433895(OCoLC)910116245(EXLCZ)99547000000243389520150526j201502 ua 0engurcn|||||||||txtrdacontentcrdamediacrrdacarrierFundamental study of a single point lean direct injector part I effect of air swirler angle and injector tip location on spray characteristics /Sarah A. Tedder [and three others]Cleveland, Ohio :National Aeronautics and Space Administration, Glenn Research Center,February 2015.1 online resource (14 pages) color illustrationsNASA/TM ;2015-218475Title from title screen (viewed on May 26, 2015)."February 2015.""Prepared for the 50th Joint Propulsion Conference cosponsored by AIAA, ASME, SAE, ASEE, Cleveland, Ohio, July 28-30, 2014."Includes bibliographical references (pages 13-14).Fundamental study of a single point lean direct injector part I Turbulent mixingnasatTurbulent combustionnasatFuel injectionnasatRecirculative fluid flownasatComputational fluid dynamicsnasatTurbulent mixing.Turbulent combustion.Fuel injection.Recirculative fluid flow.Computational fluid dynamics.Tedder Sarah A.1393138NASA Glenn Research Center,Fundamental Aeronautics Program (U.S.),GPOGPOBOOK9910703782303321Fundamental study of a single point lean direct injector part I3485103UNINA