02157nam 2200565Ia 450 991069992170332120110406162918.0(CKB)5470000002406743(OCoLC)711707571(EXLCZ)99547000000240674320110406d2010 ua 0engurmn|||||||||txtrdacontentcrdamediacrrdacarrierTransition in gas turbine control system architecture[electronic resource] modular, distributed, and embedded /Dennis Culley ; prepared for the Turbo Expo 2010 sponsored by the American Society of Mechanical Engineers (ASME), Glasgow, Scotland, United Kingdom, June 14-18, 2010Cleveland, Ohio :National Aeronautics and Space Administration, Glenn Research Center,[2010]1 online resource (11 pages) illustrations (color)NASA/TM ;2010-216806Title from title screen (viewed on April 6, 2011)."September 2010.""GT2010-23226."Includes bibliographical references (pages 10-11).Transition in gas turbine control system architecture Engine controlnasatTemperature controlnasatActive controlnasatHigh temperaturenasatControl systems designnasatDistributed parameter systemsnasatEngine designnasatCommunication networksnasatEngine control.Temperature control.Active control.High temperature.Control systems design.Distributed parameter systems.Engine design.Communication networks.Culley Dennis1392525NASA Glenn Research Center.ASME Turbo Expo(2010 :Glasgow, Scotland)GPOGPOBOOK9910699921703321Transition in gas turbine control system architecture3447356UNINA