It is so much easier now we know the context.
It's the rear spoiler ("wing" in drag-racing speak) on a ground vehicle.
Note - just put the calculation Mentalic did into the spreadsheet.
Do you follow what was done?
It would still be better to get some more data points ... the actual shape of a wing-number vs run-time would be a non-simple curve. I'd have had the three data points model as points on a parabola. This could work well if the data are close to the required ideal setting. (see links below). But you pick what you are comfortable with - it can get as complicated as you like ;)
What you need is probably best found as the relationship between lift and drag - given for aircraft.
In your case, "lift" becomes "downforce" and will act to increase traction with the ground ... allowing greater accelerations without slipping.
Drag is still the same.
To minimize your travel time, you want an angle range where the downforce-to-drag ratio is high.
If aircraft wings are anything to go by, this will actually be a range of angles.
http://www.allstar.fiu.edu/aero/lift_drag.htm
http://avstop.com/ac/flighttrainghandbook/drag.html
I don't know what the equivalent is for drag or sprint car wings off-hand - the comparison looks compelling:
See:
http://www.circletrack.com/ultimateracing/ctrp_1011_sprint_car_wing_aerodynamics/
(sprint car)
Depending on the stakes, it may be worth your while to get better data anyway.
Probably faster to binary-search the settings. You know one too high and one too low, so split the difference and try again.
I think you'll find that the other factors are so variable that a difference of a few points off ideal will not do anything to the overall time.
Seems funny that you need a computer to tell you the same thing as a pen and paper.
Personally I don't trust the things.
I think you can use the "trendline" function in exell to get you the a,b,c in the equation y=ax^2+bx+c, of the parabola that passes through all three points. (y=time, x=wing number)
After that x=-b/2a is the wing number you want.
This is a nasty estimation BTW.