Redesign Airfoil
redesign_airfoilRescale an airfoil's maximum thickness or camber by specified chord fractions using XFOIL GDES, then optionally save the modified geometry to the library under a new name.
Instructions
Rescale max thickness and/or camber (chord fractions) via XFOIL GDES TSET — the same 'modify airfoil' recipe Profili uses internally. If save_as is given, the new geometry is saved into the library under that name (and as a .dat file next to it).
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": {
"name": "<name>"
},
"name": "redesign_airfoil"
}
}Input Schema
| Name | Required | Description | Default |
|---|---|---|---|
| name | Yes | ||
| backup | No | ||
| camber | No | ||
| save_as | No | ||
| x_camber | No | ||
| thickness | No | ||
| install_dir | No | ||
| x_thickness | No |
Output Schema
| Name | Required | Description | Default |
|---|---|---|---|
| result | Yes |