neonia_aero_vspaero_solver

v0.1.0

AeroCraft AI: VSPAERO solver. Vortex lattice & panel method CFD solver computing polar curves, L/D max, static margin, and stability derivatives.

$0.015 / call (Standard Tier)

Updated: Unknown

Overview

VSPAERO aerodynamic solver. Computes Lift-to-Drag polars, static margin, and pitch/roll/yaw stability damping derivatives for UAV airframe models.

Example Input

JSON payload sent to this tool:

{
  "vsp3_path": "/path/to/uav_model.vsp3",
  "alpha_start_deg": -4.0,
  "alpha_end_deg": 12.0,
  "alpha_step_deg": 1.0,
  "mach_number": 0.05,
  "reynolds_number": 200000,
  "analysis_type": "VORTEX_LATTICE"
}

Example Output

Formatted JSON response returned by this tool:

{
  "cl_max": 1.25,
  "cd_min": 0.022,
  "ld_max": 85.2,
  "alpha_at_ld_max_deg": 4.5,
  "cl_alpha_per_deg": 0.092,
  "cm_alpha_per_deg": -0.015,
  "static_margin_pct": 12.4,
  "pitch_damping_cmq": -12.4,
  "roll_damping_clp": -0.45,
  "yaw_damping_cnr": -0.18,
  "polar_points": [
    {
      "alpha_deg": -4.0,
      "cl": -0.22,
      "cd": 0.028,
      "cm": 0.035,
      "ld": -7.86
    },
    {
      "alpha_deg": 4.5,
      "cl": 0.564,
      "cd": 0.0232,
      "cm": -0.0125,
      "ld": 24.31
    }
  ],
  "warnings": []
}

Setup Configuration

Select MCP Client

Add the following configuration to your MCP general settings or mcp_config.json:

{
  "mcpServers": {
    "neonia": {
      "serverUrl": "https://mcp.neonia.io/mcp?tools=neonia_aero_vspaero_solver",
      "headers": {
        "Authorization": "Bearer API_KEY"
      }
    }
  }
}