[HEADER]
VERSION=3

[WING_0]								; Wing identifier. A car can have as many wings as necessary.
NAME=BODY								; name of the wing
CHORD=1.0									; length of the wing in meters
SPAN=1.54								; width of the wing in meters. both help determine the frontal area of the wing. Single unit is used to simplify calculations
POSITION=0,0.10,-0.2						; 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=0.0								; Height aero lift multiplier lookup table
CL_GAIN=-0.10
LUT_AOA_CD=wing_body_AOA_CD.lut
LUT_GH_CD=
CD_GAIN=0.58
ANGLE=0
ZONE_FRONT_CL=-0.005			    ; CL=CL/(1.0+ZONE_0_CL*DAMAGE)
ZONE_FRONT_CD=0.015					; CD=CD*(1.0+ZONE_0_CD*DAMAGE)
ZONE_REAR_CL=-0.005					; CL=CL/(1.0+ZONE_0_CL*DAMAGE)
ZONE_REAR_CD=0.015					; CD=CD*(1.0+ZONE_0_CD*DAMAGE)
ZONE_LEFT_CL=-0.005					; CL=CL/(1.0+ZONE_0_CL*DAMAGE)
ZONE_LEFT_CD=0.01					; CD=CD*(1.0+ZONE_0_CD*DAMAGE)
ZONE_RIGHT_CL=-0.005				; CL=CL/(1.0+ZONE_0_CL*DAMAGE)
ZONE_RIGHT_CD=0.01					; CD=CD*(1.0+ZONE_0_CD*DAMAGE)

[WING_1]
NAME=FRONT
CHORD=1.0
SPAN=1.6
POSITION=0,-0.10,1.36
LUT_AOA_CL=wing_front_AOA_CL.lut
LUT_GH_CL=
CL_GAIN=0.1
LUT_AOA_CD=wing_front_AOA_CD.lut
LUT_GH_CD=
CD_GAIN=0
ANGLE=2
ZONE_FRONT_CL=0.015    ; CL=CL/(1.0+ZONE_0_CL*DAMAGE)

ZONE_FRONT_CD=0.015    ; 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     ; CD=CD*(1.0+ZONE_0_CD*DAMAGE)

ZONE_RIGHT_CL=0     ; CL=CL/(1.0+ZONE_0_CL*DAMAGE)

ZONE_RIGHT_CD=0     ; CD=CD*(1.0+ZONE_0_CD*DAMAGE)

[WING_2]
NAME=REAR
CHORD=1.0
SPAN=1.55
POSITION=0,0.51,-1.31
LUT_AOA_CL=wing_rear_AOA_CL.lut
LUT_GH_CL=
CL_GAIN=0.2
LUT_AOA_CD=wing_rear_AOA_CD.lut
LUT_GH_CD=
CD_GAIN=0
ANGLE=2
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=0.01     ; CL=CL/(1.0+ZONE_0_CL*DAMAGE)

ZONE_REAR_CD=0.015     ; CD=CD*(1.0+ZONE_0_CD*DAMAGE)

ZONE_LEFT_CL=0     ; CL=CL/(1.0+ZONE_0_CL*DAMAGE)

ZONE_LEFT_CD=0     ; CD=CD*(1.0+ZONE_0_CD*DAMAGE)

ZONE_RIGHT_CL=0     ; CL=CL/(1.0+ZONE_0_CL*DAMAGE)

ZONE_RIGHT_CD=0     ; CD=CD*(1.0+ZONE_0_CD*DAMAGE)


