lei-airfoil-cfd, for CFD analysis of Leading Edge Inflatable (LEI) kite airfoils.
- OpenFoam need to be installed. See https://openfoam.org/download/11-ubuntu/
Navigate to you run/ folder in your OpenFoam directory and clone the repo
run
git clone https://github.com/corentintran/lei-airfoil-cfd.git
cd lei-airfoil-cfd/
The script src/main_compute_polars run the cfd analysis. There you can specify the caracteristics of the airfoil to analyze.
The script will
- create the desired LEI airfoil geometry
- generate the mesh and store it in data/
- run openfoam on this mesh for the desired angles of attack
- generate polars plots and values and store these in the results folder.
Pull requests are welcome. For major changes, please open an issue first to discuss what you would like to change.
Specify the license under which your software is distributed, and include the copyright notice:
Beyond The Sea hereby disclaims all copyright interest in the program “lei-airfoil-cfd” generating mesh for leading edge inflatable kite airfoil and running cfd analysis on it written by the Author(s).
Copyright (c) [2024] [TRAN Corentin].