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