conda create --name airfoil python=3.8
conda activate airfoil
pip install -r requirements.txt请将数据集存放在 data 文件夹下, 默认数据集为 data/airfoil/supercritical_airfoil/*.dat
在项目的根文件夹下:
# split train/val/test
python dataload/datasplit.py
# generate parsec feature
python dataload/parsec_direct.py 在项目的根文件夹下:
# train vae, map airfoil to latent space
python train_vae.py
# train dit condition on keypoint & parsec
python train_dit.pyI have developed a baseline for editing airfoils using VAE. You can find the code here.
I have implemented a script to calculate the aerodynamic performance of airfoils, The code is available here.
I have created a demo for editing airfoils using Gradio. You can access the demo here.
I have curated a collection of papers on airfoil design. You can find the resources here.
I have intensively borrow codes from the following repositories. Many thanks to the authors for sharing their codes.