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142 lines
2.2 KiB
142 lines
2.2 KiB
# Enter a name for your vehicle
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vehicle_name: plane_example_2
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# Enter the type of airframe you would like to use:
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frame_type: custom
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# First define some model-wide parameters for custom models:
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reference_area: 12
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wing_span: 15
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# Provide a reference point at which the forces and moments generated will act.
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reference_point:
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X: 0
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Y: 0
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Z: 0
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#Provide information on each of the Control Surfaces
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num_ctrl_surfaces: 4
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control_surfaces:
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- name: right_wing
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type: aileron
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nchord: 1
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cspace: 1
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nspan: 16
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sspace: -2
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angle: 4
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translation:
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X: 0
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Y: 0
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Z: 0
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naca: 2412
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sections:
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- name: section_1
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position:
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X: -0.25
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Y: 0
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Z: 0
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chord: 1
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ainc: 0
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nspan: 8
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sspace: 1
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- name: section_2
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position:
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X: -0.175
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Y: 5
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Z: 0.5
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chord: 0.7
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ainc: 0
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nspan: 0
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sspace: 0
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- name: left_wing
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type: aileron
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nchord: 1
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cspace: 1
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nspan: 16
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sspace: -2
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angle: 4
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translation:
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X: 0
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Y: 0
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Z: 0
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naca: 2412
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sections:
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- name: section_1
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position:
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X: -0.175
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Y: -5
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Z: 0.5
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chord: 0.7
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ainc: 0
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nspan: 0
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sspace: 0
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- name: section_2
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position:
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X: -0.25
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Y: 0
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Z: 0
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chord: 1
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ainc: 0
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nspan: 8
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sspace: 1
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- name: elevator
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type: elevator
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nchord: 1
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cspace: 1
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nspan: 7
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sspace: -2
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translation:
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X: 6
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Y: 0
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Z: 0.5
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sections:
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- name: section_1
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position:
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X: -0.1
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Y: 0
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Z: 0
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chord: 0.4
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ainc: 0
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nspan: 7
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sspace: -1.25
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- name: section_2
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position:
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X: -0.075
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Y: 2
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Z: 0
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chord: 0.3
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ainc: 0
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nspan: 0
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sspace: 0
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- name: fin
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type: rudder
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nchord: 1
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cspace: 1
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nspan: 10
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sspace: 1
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translation:
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X: 6
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Y: 0
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Z: 0.5
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sections:
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- name: section_1
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position:
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X: -0.1
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Y: 0
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Z: 0
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chord: 0.4
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ainc: 0
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nspan: 7
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sspace: -1.25
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- name: section_2
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position:
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X: -0.075
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Y: 0
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Z: 1
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chord: 0.3
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ainc: 0
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nspan: 0
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sspace: 0
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