Python package to automatically analyze objects in external aerodynamic flow for a range of angle-of-attack
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 https://github.com/inflowencer/pyaoa.git ~/
Four examples are provided in the examples directory.
- Subsonic NACA0012 in SU2
- Transonic RAE2822 in OpenFOAM
- Subsonic Selig S1210 in Fluent
- High-lift airfoil variations in SU2
See the Quickstart.
Download the file for your platform. If you're not sure which to choose, learn more about installing packages.