Aero-Thermodynamic Model for13; Digital Simulation of13; Turbo of an Engine

Kapadi, Yogesh and Pashilkar, AA (2005) Aero-Thermodynamic Model for13; Digital Simulation of13; Turbo of an Engine. Technical Report. National Aerospace Laboratories, Bangalore, India.

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    Prediction of engine performance over the flight envelope at an early design stage13; is important for new engine development and also for the controller design. The13; document covers the development and validation of an aero-thermodynamic model13; for a twin-spool mixed flow turbofan engine based on the state variable and control13; volume approach. Using component performance data, engine simulation models13; are developed for steady state and transient simulation in MATLAB-SIMULINK. The13; results are validated against an independent software called Gas turbine Simulation13; Program (GSP). This turbofan engine model can be used for the development of13; Integrated Flight and Propulsion Control (IFPC) systems.

    Item Type: Proj.Doc/Technical Report (Technical Report)
    Uncontrolled Keywords: Component characteristics;Off design analysis;Transient simulation
    Subjects: AERONAUTICS > Avionics & Aircraft Instrumentation
    Division/Department: Flight Mechanics and Control Division, Flight Mechanics and Control Division
    Depositing User: Mrs Manoranjitha M D
    Date Deposited: 16 Jan 2009
    Last Modified: 27 Aug 2015 12:01

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