Theory of aircraft turbine engines

Garant předmětu:

Lecturer:

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Department of Mechanics, Biomechanics and Mechatronics

Synopsis:

•Thermodynamic cycles of turbine engines, optimization of thermodynamic cycles.

•Axial compressor - characteristics, aerodynamics.

•Axial compressor - design layout.

•Axial compressor - stability, surge.

•5, Radial compressor.

•Combustion chamber.

•Turbine - characteristics, aerodynamics, design.

•Nozzle and exhaust.

•Simulation and optimization methods for turbine engines.

•1D methods (NPSS) - basics, theory, usage, mathematical model.

•2D methods - simulation in planes S1, S2.

•Throughflow calculation.

•Model verification and tuning, model based on experimental data.

•Noise and its reduction.

Requirements:

Syllabus of lectures:

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Study materials:

•Farokhi S.: Aircraft Propulsion, Wiley, ISBN 9781118806777, 2014

•Sultanian B. K., Gas Turbines: Internal Flow Systems Modelling, Cambridge, ISBN 978-1-107-17009-4, 2018

•Aungier R. H.: Axial Flow Compressors: A Strategy for Aerodynamic Design and Analysis, Wiley, ISBN 978-

1860584220, 2003

•Bräunling W. J. G.: Flugzeugtriebwerke, Springer, ISBN 978-3-540-76368-0, 2015

Note:

Further information:

No time-table has been prepared for this course

The course is a part of the following study plans: