pterasim.simulate
Calculate aerodynamic coefficients for wing simulations. Input wing geometry, flapping schedule, and timesteps to receive force, torque, and solver data for flight analysis.
Instructions
Generate aerodynamic coefficients with UVLM fallback. Supply wing geometry, flapping schedule, and timestep count. Returns forces, torques, and solver metadata. Example: {"span_m":0.8,"chord_m":0.12,"num_timesteps":180}
Input Schema
| Name | Required | Description | Default |
|---|---|---|---|
| request | Yes |
Input Schema (JSON Schema)
{
"properties": {
"request": {
"$ref": "#/$defs/PterasimInput"
}
},
"required": [
"request"
],
"type": "object"
}