01779nam 2200505I 450 991070481680332120131113164317.0(CKB)5470000002445571(OCoLC)862949255(EXLCZ)99547000000244557120131113d2013 ua 0engurcn|||||||||txtrdacontentcrdamediacrrdacarrierAdvanced shock 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 (12 pages) illustrationsNASA/TM ;2013-216515Title from title screen (viewed Nov. 13, 2013)."May 2013."Includes bibliographical references (pages 11-12).Inlet flownasatControllersnasatFeedback controlnasatComputerized simulationnasatTurbine enginesnasatEngine inletsnasatInlet flow.Controllers.Feedback control.Computerized simulation.Turbine engines.Engine inlets.Csank Jeffrey T.1402819Stueber Thomas J.Fundamental Aeronautics Program (U.S.),NASA Glenn Research Center,GPOGPOBOOK9910704816803321Advanced shock position control for mode transition in a turbine based combined cycle engine inlet model3512465UNINA