create_naca4_airfoil
Generate NACA 4-digit airfoil geometries as 2D profiles or 3D solids by supplying airfoil code, chord, span, and point count.
Instructions
Create a NACA 4-digit airfoil (3D solid if span>0, 2D profile if span=0).
Tool call template
Replace each placeholder with a value matching the input schema. Only required parameters are included; add optional parameters as needed.
{
"id": 1,
"jsonrpc": "2.0",
"method": "tools/call",
"params": {
"arguments": {
"code": "<code>"
},
"name": "create_naca4_airfoil"
}
}Input Schema
| Name | Required | Description | Default |
|---|---|---|---|
| code | Yes | ||
| name | No | ||
| span | No | ||
| chord | No | ||
| n_points | No | ||
| closed_te | No |
Output Schema
| Name | Required | Description | Default |
|---|---|---|---|
| result | Yes |