Analyze Airfoil
analyze_airfoilComputes a viscous airfoil polar using bundled XFOIL and optionally saves results to the Profili library for GUI access.
Instructions
Compute a fresh viscous polar with the bundled XFOIL (same recipe as Profili's own solver). If save_to_db=True the result is written into the Profili library and appears in the GUI after restart.
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": "analyze_airfoil"
}
}Input Schema
| Name | Required | Description | Default |
|---|---|---|---|
| re | No | ||
| mach | No | ||
| name | Yes | ||
| ncrit | No | ||
| backup | No | ||
| alfa_end | No | ||
| alfa_step | No | ||
| alfa_start | No | ||
| save_to_db | No | ||
| install_dir | No |
Output Schema
| Name | Required | Description | Default |
|---|---|---|---|
| result | Yes |