02167nam 2200553I 450 991070248600332120130128091620.0(CKB)5470000002427305(OCoLC)825550608(EXLCZ)99547000000242730520130128d2012 ua 0engurcn|||||||||txtrdacontentcrdamediacrrdacarrierA turbine based combined cycle engine inlet model and mode transition simulation based on HiTECC tool /Jeffrey T. Csank and Thomas J. StueberCleveland, Ohio :National Aeronautics and Space Administration, Glenn Research Center,2012.1 online resource (13 pages) color illustrationsNASA/TM ;2012-217714Title from title screen (viewed on Jan. 14, 2013)."September 2012.""Prepared for the 48th Joint Propulsion Conference and Exhibit cosponsored by AIAA, ASME, SAE, and ASEE Atlanta, Georgia, July 30 to August 1, 2012.""AIAA-2012-4149."Includes bibliographical references (pages 12-13).Computerized simulationnasatPropulsion system configurationsnasatWind tunnel testsnasatFuel systemsnasatPropulsion system performancenasatTurbine enginesnasatEngine inletsnasatComputerized simulation.Propulsion system configurations.Wind tunnel tests.Fuel systems.Propulsion system performance.Turbine engines.Engine inlets.Csank Jeffrey T.1402819Stueber Thomas J.NASA Glenn Research Center,Joint Propulsion Conference and Exhibit(48th :2012 :Atlanta, Ga.)GPOGPOBOOK9910702486003321A turbine based combined cycle engine inlet model and mode transition simulation based on HiTECC tool3489481UNINA