https://github.com/inflowencer/pyaoa
Python package to automatically analyze objects in external aerodynamic flow for a range of angle-of-attack
https://github.com/inflowencer/pyaoa
cfd
Last synced: 5 months ago
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Python package to automatically analyze objects in external aerodynamic flow for a range of angle-of-attack
- Host: GitHub
- URL: https://github.com/inflowencer/pyaoa
- Owner: inflowencer
- License: mit
- Created: 2022-09-01T08:32:05.000Z (almost 4 years ago)
- Default Branch: master
- Last Pushed: 2022-10-08T17:50:29.000Z (over 3 years ago)
- Last Synced: 2025-09-20T16:06:08.177Z (9 months ago)
- Topics: cfd
- Language: Python
- Homepage:
- Size: 1.38 MB
- Stars: 0
- Watchers: 1
- Forks: 0
- Open Issues: 0
-
Metadata Files:
- Readme: README.md
- License: LICENSE
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README
# 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
```sh
pip install pyaoa
```
## Examples
Clone the repository which includes the examples:
```sh
git clone https://github.com/inflowencer/pyaoa.git ~/
```
Four examples are provided in the [examples](examples/) directory.
1. [Subsonic NACA0012](examples/NACA0012/) in SU2
2. [Transonic RAE2822](examples/RAE2822/) in OpenFOAM
3. [Subsonic Selig S1210](examples/S1210) in Fluent
4. [High-lift airfoil variations](examples/NACA0056mod) in SU2
## Userguide
See the [Quickstart](doc/README.md).