Aerodynamics

3 Credits

Application of fluid dynamics to flows past lifting surfaces, and inside nozzles and diffusers. Fundamentals of potential flow are covered including: the Kutta-Joukowski theorem, physical basis for the Kutta condition, thin airfoil theory, sectional pressure profiles and separation, and lifting line theory. Compressible isentropic subsonic/supersonic and non-isentropic supersonic flows are covered including: supersonic airfoils, shock waves, shock reflections, and expansion fans. Credit will not be given for both MECH 326 and MECH 426 . Prerequisites: ME 231