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Python package to automatically analyze objects in external aerodynamic flow for a range of angle-of-attack

Project description

pyaoa - Automatic Angle-of-Attack Analysis

Automatic pre- and postprocessing of external aerodynamic simulations of arbitrary numbers of objects to analyze at different angles-of-attack $\alpha$ in your preferred CFD solver.


pip install pyaoa


Clone the repository which includes the examples:

git clone ~/

Four examples are provided in the examples directory.

  1. Subsonic NACA0012 in SU2
  2. Transonic RAE2822 in OpenFOAM
  3. Subsonic Selig S1210 in Fluent
  4. High-lift airfoil variations in SU2


See the Quickstart.

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