use xfoil calculate Cl/Cd performance in Linux
conda create --name airfoil python=3.8
conda activate airfoil
pip install -r requirements.txt
- Download the airfoil dataset here
- ln -s /home/bingxing2/ailab/scxlab0059/data/airfoil/cst_gen cst_gen
chmod +x xfoil
- python calc.py --s xx --e xx