01616nam 2200457I 450 991071306670332120200319134032.0(CKB)5470000002499534(OCoLC)1145279742(EXLCZ)99547000000249953420200319j202003 ua 0engur|||||||||||txtrdacontentcrdamediacrrdacarrierFuel flexible combustor for high-OPR compact-core N+3 propulsion engine final technical report /Lance L. SmithCleveland, Ohio :National Aeronautics and Space Administration, Glenn Research Center,March 2020.1 online resource (91 pages) illustrations (mostly color)NASA/CR ;2020-220489"March 2020."Includes bibliographical references (page 91).Fuel flexible combustor for high-OPR compact-core N+3 propulsion engine Bypass rationasatComputational fluid dynamicsnasatCombustion chambersnasatHigh pressurenasatDynamic testsnasatBypass ratio.Computational fluid dynamics.Combustion chambers.High pressure.Dynamic tests.Smith Lance L.1394506NASA Glenn Research Center,GPOGPOBOOK9910713066703321Fuel flexible combustor for high-OPR compact-core N+3 propulsion engine3452010UNINA