Course Contents
Contents
compressible Flows: stream filament theory, shock waves, Prandtl-Meyer
expansions, gas dynamic equations, aerofoil 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
Anderson JD, Modern Compressible Flow, McGraw Hill, 1990
Preconditions
Aerodynamik I
- Lehrende: Jeanette Hussong
Semester: SoSe 2024