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

  1. Governing Equations for Compressible Potential Flow

  2. Types of Partial Differential Equations

  3. 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

  4. Singularity Method

  5. Outer potential flow over a thin profile at zero lift
    1. Incompressible: Singularity Method