AAE 51400 - Intermediate Aerodynamics

Credit Hours: 3.00. Thin airfoil theory and panel methods. Three-dimensional elementary solutions, lifting-line and lifting-surface models. Slender wing and slender body theory. Normal/oblique shock waves. One- and multi-dimensional flows and conical flows. Method of characteristics. Introduction to transonic flow, hypersonic flow, and airfoil design. Credits: 3.00