Uiuc Airfoil Geometry
uiuc_airfoil_geometryFetch one airfoil's coordinate file live from the UIUC Airfoil Coordinates Database (University of Illinois Urbana-Champaign, Applied Aerodynamics Group) and compute its geometry: point count, max thickness and max camber (each as a fraction of chord, with the chordwise location they occur at), derived from the raw (x,y) coordinates. Pass the airfoil's name as listed by uiuc_airfoil_search (e.g. "naca2412", "e58", "s1223").
Input Schema
| Name | Required | Description | Default |
|---|---|---|---|
| name | Yes | Airfoil name, e.g. "naca2412" or "s1223" | |
| include_coordinates | No | Include the full raw (x,y) point list in the response (default false — only the summary geometry) |