[HEADER]
VERSION=0.9

[WING_0]                                ; Wing identifier. A car can have as many wings as necessary.
NAME=BODY                                ; name of the wing
CHORD=2.55                                   ; length of the wing in meters
SPAN=2.5                                ; width of the wing in meters. both help determine the frontal area of the wing. Single unit is used to simplify calculations
POSITION=0,0.6,0                        ; 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=1.0                                ; 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=1.0                                ; Coefficient of drag multiplier (for easy fine tuning)
ANGLE=0   

[WING_1]
NAME=FRONT WING
CHORD=0.45
SPAN=2.4
POSITION=0,-0.50,2.235
LUT_AOA_CL=front_wing_AOA_CL.lut
LUT_GH_CL=			
CL_GAIN=1.1
LUT_AOA_CD=front_wind_AOA_CD.lut
LUT_GH_CD=					
CD_GAIN=0.925
ANGLE=3

[WING_2]
NAME=ROOF WING
CHORD=0.35
SPAN=1.5
POSITION=0,1.685,0.675
LUT_AOA_CL=roof_wing_AOA_CL.lut
LUT_GH_CL=							
CL_GAIN=1.1
LUT_AOA_CD=roof_wing_AOA_CD.lut
LUT_GH_CD=					
CD_GAIN=0.9
ANGLE=24