pyaoa 0.2

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.

Installation

pip install pyaoa

Examples

Clone the repository which includes the examples:

git clone https://github.com/inflowencer/pyaoa.git ~/

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

Userguide

See the Quickstart.