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Degree

Gas Turbine Propulsion

Principles of aerospace propulsion systems and their classification. Basic principles of boundary layer mechanics and heat transfer. Cycle analysis: Thermodynamics of air breathing engines. Aero-thermodynamics of non-rotating propulsion components: inlets, combustors and nozzles Turbo-machinery : Axial compressors and turbines; centrifugal pumps and compressors.

Code BSAS4003
Credits 4 Credits
Type Course
Prerequisites None