generate_airfoil_geometry
Generates NACA 4/5-digit airfoil geometry and returns a reusable geometry ID for CFD analysis.
Instructions
Generate a NACA 4/5-digit airfoil geometry and return a reusable geometry_id.
Input Schema
| Name | Required | Description | Default |
|---|---|---|---|
| naca_code | Yes | NACA 4- or 5-digit airfoil code, for example '0012' or '23012'. | |
| chord_length | No | Airfoil chord length in meters. | |
| n_points_per_side | No | Number of coordinate points sampled on each airfoil side. | |
| normalize_geometry | No | Normalize the generated airfoil to unit chord before scaling. |
Output Schema
| Name | Required | Description | Default |
|---|---|---|---|
No arguments | |||