[HEADER]
VERSION=0.9


[WING_0]								; Wing identifier. A car can have as many wings as necessary.
NAME=BODY								; name of the wing
CHORD=11.0									; length of the wing in meters
SPAN=2.4								; width of the wing in meters. both help determine the frontal area of the wing. Single unit is used to simplify calculations
POSITION=0,-0.5,-0.5						; 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=0.80								; Coefficient of drag multiplier (for easy fine tuning)
ANGLE=0								; Default starting wing angle (degrees)
ZONE_FRONT_CL=0     ; CL=CL/(1.0+ZONE_0_CL*DAMAGE)
ZONE_FRONT_CD=0    ; CD=CD*(1.0+ZONE_0_CD*DAMAGE)
ZONE_REAR_CL=0     ; CL=CL/(1.0+ZONE_0_CL*DAMAGE)
ZONE_REAR_CD=0     ; CD=CD*(1.0+ZONE_0_CD*DAMAGE)
ZONE_LEFT_CL=0     ; CL=CL/(1.0+ZONE_0_CL*DAMAGE)
ZONE_LEFT_CD=0.01     ; CD=CD*(1.0+ZONE_0_CD*DAMAGE)
ZONE_RIGHT_CL=0     ; CL=CL/(1.0+ZONE_0_CL*DAMAGE)
ZONE_RIGHT_CD=0.01     ; CD=CD*(1.0+ZONE_0_CD*DAMAGE)
