01973nam 2200493I 450 991070462220332120140206155449.0(CKB)5470000002443496(OCoLC)869945627(EXLCZ)99547000000244349620140206d2013 ua 0engurcn|||||||||txtrdacontentcrdamediacrrdacarrierShock position control for mode transition in a turbine based combined cycle engine inlet model /Jeffrey T. Csank and Thomas J. StueberCleveland, Ohio :National Aeronautics and Space Administration, Glenn Research Center,2013.1 online resource (17 pages) color illustrationsNASA/TM ;2013-217824Title from title screen (viewed on Feb. 6, 2014)."January 2013.""Prepared for the 45th Combustion/33rd Airbreathing Propulsion/33rd Exhaust Plume and Signatures/27th Propulsion Hazards Joint Subcommittee Meeting sponsored by the Joint Army-Navy-NASA-Air Force (JANNAF), Monterey, California, December 3-7, 2012."Includes bibliographical references (pages 16-17).Computerized simulationnasatEngine inletsnasatFeedback controlnasatInlet flownasatTurbine enginesnasatComputerized simulation.Engine inlets.Feedback control.Inlet flow.Turbine engines.Csank Jeffrey T.1402819Stueber Thomas J.NASA Glenn Research Center,Fundamental Aeronautics Program (U.S.),GPOGPOBOOK9910704622203321Shock position control for mode transition in a turbine based combined cycle engine inlet model3520142UNINA