Aerodynamics
Screen wing loads, airfoil behavior, induced drag, and static stability.
AS-AE-04
Available calculations.
- wing_vlm_analysis
- airfoil_polar_analysis
- calculate_stability_derivatives
- get_airfoil_database
Runner example.
The installed skill teaches your agent when to activate this module and how to call the local runner.
wing_vlm_analysisAS-AE-04
{
"ok": true,
"operation": "wing_vlm_analysis",
"result": {
"lift_coefficient": 0.504969,
"drag_coefficient": 0.035252,
"induced_drag_coefficient": 0.013252,
"lift_n": 10819.4,
"drag_n": 755.31,
"aspect_ratio": 7.469,
"lift_to_drag": 14.324
},
"units": {
"lift_n": "N",
"drag_n": "N"
},
"assumptions": [
"Incompressible finite-wing lifting-line approximation",
"Elliptic loading represented through Oswald efficiency"
],
"warnings": [
"Preliminary analysis only; not a substitute for CFD, wind-tunnel, or flight-test data"
],
"provenance": [
"Prandtl finite-wing lift slope and induced-drag relations"
]
}