Kapadi, Yogesh and Pashilkar, Abhay (2005) Aero-Thermodynamic Model for13; Digital Simulation of13; Turbo of an Engine. Technical Report. National Aerospace Laboratories, Bangalore, India.
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Abstract
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: | 24 May 2010 09:40 |
| URI: | http://nal-ir.nal.res.in/id/eprint/1013 |
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