VU Computational Aerodynamics, 322.079

For the description of the course and registration, see TISS.

Course organization

Lecture videos

Lecture notes

1. Introduction to Computational Aerodynamics

Part A: Analysis

2. Governing Equations for Compressible Potential Flow

3. Compressible potential flow over a thin airfoil

   • Asymptotic Expansion

4. Types of Partial Differential Equations

5. Supersonic potential flow over a thin airfoil at zero lift

6. Singularity Method

7. Boundary-Layer Theory

   1. Boundary-Layer Equations

   2. Boundary-Layer Effects

   3. Similar Solutions of the Boundary-Layer Equations

   4. Numerical Solution of the Falkner-Skan Equation

   5. Momentum-Integral Equation