Conceptual Design and Development of Jet Aircraft Engine Turbines

Course guarantor:

Lecturer:

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Supervisor:

Department of Aerospace Engineering

Synopsis:

Aerodynamic, thermodynamic and thermo-physic processes, criteria of physical similarity. Computational and experimental methods. Experimental conceptions from research of blade cascades, testing models and experimental machines. Cooling system of stator and rotor blades. Heat-resisting materials and special technologies.

Requirements:

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Study materials:

1. Kamenický J.: Aircraft Turbo Engines Design, VAAZ Brno, U781/2, 1989

2. Mattingly J. D.: Aircraft Engine Design, University of Washington, 2002

3. Journal of Propulsion and Power

4. AIAA Journal

5. Journal of Thermo physics and Heat Transfer

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Further information:

No time-table has been prepared for this course

The course is a part of the following study plans: