This project automates the workflow for NACA 4-digit airfoil analysis and converts mathematical results into 3D CAD geometries. It bridges the gap between Python-based aerodynamic calculations and SolidWorks/CATIA modeling.
Below is a 3D render of a wing section generated using this automation tool, showing the high-precision profile transition.
- NACA Profile Generation: Automates the geometry calculation for any 4-digit NACA airfoil.
- System Automation: Bash scripting (
analiz_merkezi.sh) to streamline data export and processing. - 3D Modeling Integration: Generates coordinate point clouds optimized for SolidWorks "Curve Through XYZ Points" feature.
- Structural Consideration: Designed for internal spar and rib integration.
- Languages: Python (Numerical Analysis), Bash (Automation)
- CAD Tools: SolidWorks / CATIA
- Environment: WSL2 / Ubuntu Linux on Windows
- kanat_raporu.py: The core engine for aerodynamic calculations.
- analiz_merkezi.sh: The "control center" script for automation.
- kati_model.py: Generates the 3D-ready coordinate data.
Alperen - Mechanical Engineering Student | Aspiring Aerospace Engineer