02171nam 2200529I 450 991070467170332120130712130528.0(CKB)5470000002442996(OCoLC)852691220(EXLCZ)99547000000244299620130712d2012 ua 0engurmn|||||||||txtrdacontentcrdamediacrrdacarrierHighlights from a Mach 4 experimental demonstration of inlet mode transition for Turbine-Based Combined Cycle hypersonic propulsion /Lancert E. Foster [and three others]Cleveland, Ohio :National Aeronautics and Space Administration, Glenn Research Center,2012.1 online resource (13 pages) illustrations (some color)NASA/TM ;2012-217724Title from title screen (viewed on July 12, 2013)."December 2012.""Prepared for the Joint Propulsion Conference and Exhibit cosponsored by AIAA, ASME, SAE, ASEE, Atlanta, Geogria, July 30 to August 1, 2012."Includes bibliographical references (page 13).Engine inletsnasatHypersonic flightnasatSupersonic speednasatAir breathing enginesnasatSupersonic combustion ramjet enginesnasatSpecific impulsenasatPropulsion system configurationsnasatEngine inlets.Hypersonic flight.Supersonic speed.Air breathing engines.Supersonic combustion ramjet engines.Specific impulse.Propulsion system configurations.Foster Lancert E.1415668NASA Glenn Research Center,Joint Propulsion Conference and Exhibit(48th :2012 :Atlanta, Ga.),GPOGPOBOOK9910704671703321Highlights from a Mach 4 experimental demonstration of inlet mode transition for Turbine-Based Combined Cycle hypersonic propulsion3518382UNINA