Anwendung strömungsmechanischer Berechnungsverfahren in Flugtriebwerken

What it is about

In this module you will learn flow-mechanical calculation methods specifically for jet propulsion. You will engage with the individual components (inlet, compressor, combustion chamber, turbine, nozzle) and the associated flow models, and you will acquire the ability to treat flows in Meridian (S2) and profile grid surfaces (S1) computationally.

What you will be able to do

• Understanding of the components of jet propulsion
• Mastery of mathematical fundamentals of fluid mechanics (vector and tensor calculus)
• Application of conservation laws, stress–strain relations and turbulence models
• Computational methods for flow in the Meridian surface (S2 surface)
• Methods for calculating profile-grid flow (S1 surface)
• Knowledge of similarity considerations, key figures and field quantities
• Fundamentals of turbomachinery, including absolute-relativistic system and turbine equation

What the module consists of

• VorlesungConveying the content through lecture and presentation; slide deck and online material to support own notes

Teaching method

• Vortrag/Präsentationfor structured conveyance of the learning content
• Online teaching materials / slide collectionfor review and as a basis for own notes