An interactive tool that uses a Deep Learning surrogate model to predict aerodynamic performance and perform inverse design optimization.
-
Instant Inference: Predicts
$C_L$ and$C_D$ using a trained neural network. -
Inverse Optimization: Automatically suggests NACA parameters (
$m, p, t$ ) to meet a user-defined Target$C_L$ . - Validation: Integrates with XFOIL via AeroSandbox to visualize real-world geometry and performance polars.
- Python 3.x
- XFOIL (You must download this separately)
- Install dependencies:
pip install -r requirements.txt - Update the
XFOIL_PATHvariable inAirfoil_Design_App.pyto point to yourxfoil.exe. - Run the application:
python Airfoil_Design_App.py