FoilMesh/example.json at master · Zcaic/FoilMesh · GitHub

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{
  "Airfoil_file":"./optimized_airfoil.dat",
  "Airfoil_data":null,
  "Output": "./Mesh/mesh.su2",
  "Spline_refine": {
    "Refinement tolerance": 172.0,
    "Refine trailing edge old": 3,
    "Refine trailing edge new": 6,
    "Refine trailing edge ratio": 3,
    "Number of points on spline": 200
  },
  "Trailing_edges":false,
  "Trailing_control": {
    "Upper side blending length": 30.0,
    "Lower side blending length": 30.0,
    "Upper blending polynomial exponent": 3,
    "Lower blending polynomial exponent": 3,
    "Trailing edge thickness relative to chord": 0.4
  },
  "Airfoil_mesh": {
    "Divisions normal to airfoil": 15,
    "1st cell layer thickness": 0.004,
    "Cell growth rate": 1.05
  },
  "Trailing_mesh": {
    "Divisions at trailing edge": 3,
    "Divisions downstream": 15,
    "1st cell layer thickness": 0.004,
    "Cell growth rate": 1.05
  },
  "Windtunnel_airfoil": {
    "Windtunnel height": 3.5,
    "Divisions of tunnel height": 100,
    "Cell thickness ratio": 10.0,
    "Distribution biasing": "symmetric",
    "Smoothing algorithm": "elliptic",
    "Smoothing iterations": 20,
    "Smoothing tolerance": 1.2e-5
  },
  "Windtunnel_wake": {
    "Windtunnel wake": 7.0,
    "Divisions in the wake": 100,
    "Cell thickness ratio": 15.0,
    "Equalize vertical wake line at": 30.0
  }
}