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. Compressible Potential Flow Over a Thin Airfoil: Asymptotic Expansion

  3. Types of Partial Differential Equations

  4. Supersonic Potential Flow Over a Thin Airfoil at Zero Lift: D'Alembert Solution

  5. Singularity Method for Incompressible Potential Flows

  6. Subsonic Potential Flow Over a Thin Airfoil at Zero Lift: Prandtl-Glauert Mapping
  7. Thin Airfoil Theory: Circulation and Lift
  8. 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

Part B: Pre-CFD Numerical Methods

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