Application of Fluidmechanic Calculation Methods for Flight Propulsion
Anwendung strömungsmechanischer Berechnungsverfahren in Flugtriebwerken
Course 249983417 in WS 2022/3
General Data
Course Type | lecture |
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Semester Weekly Hours | 2 SWS |
Organisational Unit | Chair of Turbomachinery and Flight Propulsion (Prof. Gümmer) |
Lecturers |
Nina Wolfrum Responsible/Coordination: Volker Gümmer Assistants: Jonas Schroeter |
Dates |
Fri, 08:00–11:00, MW 0608M |
Assignment to Modules
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MW0147: Anwendung strömungsmechanischer Berechnungsverfahren in Flugtriebwerken / Application of Fluid-Mechanical Computational Methods in Aero Engines
This module is included in the following catalogs:- Catalogue of non-physics elective courses
Further Information
Courses are together with exams the building blocks for modules. Please keep in mind that information on the contents, learning outcomes and, especially examination conditions are given on the module level only – see section "Assignment to Modules" above.
additional remarks | - Review of the basic equations of fluid mechanics. - Overview of calculation methods used in turbomachinery - Introduction to S1 and S2 methods - Methodical basics of blade and annulus geometry generation - Introduction to 3D CFD methods of multi-stage turbomachinery - Importance and implementation of turbomachine-relevant meshing aspects and meshing techniques - Turbomachinery-specific boundary conditions: Wall treatment, non-reflecting edges, rotor-stator interface. - Turbulence and transition modeling in the context of multistage simulation - Interdisciplinary CFD aspects: Flutter and forced-response evaluation of blades, heat transfer calculations. - Frequency domain methods for transient treatment of flow in multi-domain arrangements - Post-processing of result data from steady-state and time-accurate engine simulations - Introduction to numerical optimization and probabilistic approaches - Introduction to Lattice-Boltzmann methods |
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Links |
Course documents E-Learning course (e. g. Moodle) TUMonline entry |