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Instructors: Prof. Dr.-Ing. Jeanette Hussong
Event type:
Lecture
Org-unit: Dept. 16 - Mechanical Engineering
Displayed in timetable as:
Aerodynamics II
Subject:
Crediting for:
Hours per week:
3
Language of instruction:
Englisch
Min. | Max. participants:
- | -
Course Contents:
Contents
compressible Flows: stream filament theory, shock waves, Prandtl-Meyer
expansions, gas dynamic equations, airfoil theory, lifting-line theory,
compressible boundary layers
Learning Outcomes
Students will be able to compute the compressible flow field around airfoils,
wings and fuselages, including the main aerodynamic coefficients (forces
and moments). If necessary the influence of the boundary layer can be taken
into consideration. The method of characteristics will be familiar as a
tool for computing more complex geometries
Literature:
Tropea/Grundmann Aerodynamik II (Shaker Verlag), erhältlich im Sekretariat
des Fachgebiets Strömungslehre und Aerodynamik
Anderson JD, Modern Compressible Flow, McGraw Hill, 1990
Preconditions:
Aerodynamik I
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