[HEADER]
VERSION=2



[WING_0]								; Wing identifier. A car can have as many wings as necessary.
NAME=BODY								; name of the wing
CHORD=2									; length of the wing in meters
SPAN=1.47								; width of the wing in meters. both help determine the frontal area of the wing. Single unit is used to simplify calculations
POSITION=0,0.88,-0.6						; position in x,y,z starting from the CoG
LUT_AOA_CL=wing_body_AOA_CL.lut			; Coefficient of Lift lookup table
LUT_GH_CL=								; Height aero lift multiplier lookup table
CL_GAIN=0.1									; Coefficient of Lift multiplier (for easy fine tuning) 
LUT_AOA_CD=wing_body_AOA_CD.lut			; Coefficient of drag lookup table
LUT_GH_CD=								; Height aero drag multiplier table
CD_GAIN=0.7								; Coefficient of drag multiplier (for easy fine tuning)
ANGLE=0									; Default starting wing angle (degrees)



[WING_1]
NAME=REAR
CHORD=0.2
SPAN=1.20
POSITION=0,0.80,-2.2
LUT_AOA_CL=wing_rear_AOA_CL.lut
LUT_GH_CL=
CL_GAIN=1
LUT_AOA_CD=wing_rear_AOA_CD.lut
LUT_GH_CD=
CD_GAIN=0.25
ANGLE=1



[WING_2]
NAME=FRONT
CHORD=0.5
SPAN=1.69
POSITION=0,0.30,1.68
LUT_AOA_CL=wing_front_AOA_CL.lut
LUT_GH_CL=
CL_GAIN=0
LUT_AOA_CD=wing_front_AOA_CD.lut	
LUT_GH_CD=
CD_GAIN=1
ANGLE=0