01727oam 2200469I 450 991071359040332120200925144444.0(CKB)5470000002501756(OCoLC)1153938334(OCoLC)995470000002501756(EXLCZ)99547000000250175620200511j202004 ua 0engur|||||||||||txtrdacontentcrdamediacrrdacarrierCombustion dynamics characteristics and fuel pressure modulation responses of a three-cup third-generation swirl-venturi lean direct injection combustion concept /Zhuohui J. He [and five others]Cleveland, Ohio :National Aeronautics and Space Administration, Glenn Research Center,April 2020.1 online resource (9 pages) color illustrationsNASA/TM ;2020-220522"April 2020."Includes bibliographical references (page 9).Fuel injectionnasatCombustionnasatCombustion chambersnasatNoise measurementnasatFuel-air rationasatFuel injection.Combustion.Combustion chambers.Noise measurement.Fuel-air ratio.He Zhuohui J.1403836NASA Glenn Research Center,GPOGPOGPOBOOK9910713590403321Combustion dynamics characteristics and fuel pressure modulation responses of a three-cup third-generation swirl-venturi lean direct injection combustion concept3477247UNINA