After successful completion of the course, students are able to:
Gas dynamics: Introductory concepts, fundamental definitions and equations, speed of sound, Mach number, thermodynamics; Steady isoentropic flow, choked flow, subsonic and supersonic nozzles; De-Laval nozzle, Hugoniot equations; Flow with friction, Fanno line; Flow with heat addition, Rayleigh line; Shock waves, conservation relations, normal and oblique shocks. Aerodynamics: external flows, aerodynamic forces and moments; skin friction, pressure drag and lift; incompressible flow around an airfoil; NACA airfoils; modern low-speed NASA airfoils; Finite wings; Linear theory for subsonic and supersonic compressible flow over an airfoil; elements of hypersonic flow. All themes will be illustrated via examples and exercises.
The following methods will be used to support students in achieving the expected learning outcomes:
Registration to the course is required
Suggested Readings:John D. Anderson, Fundamentals of Aerodynamics. Sixth edition. New York: McGraw-Hill Science/Engineering/Math 2017.
Hans Wolfgang Liepmann, Anatol Roshko, Elements of Gasdynamics. Dover Books on Aeronautical Engineering Series, Courier corporation 2001.
Students have to write a final exam to assess whether they have achived the expected knowledge and preparation.