QUOTE (insta @ Sep 2 2006, 01:43 AM)

You forgot one thing though, CG. Your calculations are for an airfoil, not a static obstruction in the airstream. You're essentially talking about mounting an upside-down aircraft wing to a car, which isnt' what's done.
Rather, consider a piece of unfoiled metal 5 feet wide, one foot deep, proped at a 45 degree angle. You end up with a frontal face of 0.84 ft x 5ft wide. Surface area is roughly 4.25 ft^2. Assuming an airspeed velocity of 100ft/sec (just under 70mph), we end up with 4250 ft^3/sec traveling past this wing.
Air has a mass of 0.080 lbs/ft^3 (
source). Assuming a near-perfect deflection (which could be possible given eddies caused by the car's body and vacuum behind the wing), the downforce from the wing alone is
340lbs! Nearly 15% of the vehicle's loaded weight, and it's concentrated in the rear alone. That's just the F=ma number from the wing having to push that much air upwards.
Of course, you also now have to contend with drag. My paper-napkin math shows me it's roughly 200 lbs of drag trying to pull the car to a stop. Here's what I came up with, please feel free to double-check me. The ZX2 at 4000 RPM in 4th gear should be traveling around 70mph:
(4000 revolutions per minute / (.98 ratio * 4.10 differential)) * 2ft diameter tire * 3.14 / 5280 ft per mile * 60 minutes per hour = 71 miles an hour. Looking at a
ZX2 Dyno, you can see they pull about 85hp at 4000 RPM, which is 111ft/lbs of torque. Multiply the torque by the gear ratio, and you end up with 446ft/lbs of torque at the axle. Divide it by the diameter of the tire, and the ZX2 produces 223 lbs of motive force in 4th gear at the rubber of the road.
It will be able to maintain speed with that large of a wing, and receive a significant additional shove downwards.
well, the original discussion, i thought, was about "wings" (of which the stuff i talked about early covers, and are relativly useless at angles greater then about 16 deg{ that is CL falls of after about 16 deg) not "surfaces" that are subjected to airflow. so ill bite on this...

....this is @ 70 mph with a "surface" (aka "duck tail") area of 10ft. sq. at an angle of 45 deg. and treating air (which is a fluid) as if it were a solid and at an altitude of 0 feet with "standard atmospheric conditions". [also, you must remember that a pound of force is not equal to a pound of mass] of course, this theory holds true if you were throwing rocks at the "surface". but air is a fluid, not a soild. Fluids exhibit different mechnical properties then that of a solid. good thought tho. the thing with the theory of having a "duck tail" is that you create higher pressure on top of the surface creating a pressure difference just like that of a wing. (as angle increases CL falls off after about 16 deg while CD continous to increase for the surface). you would find that the drag of an airfoil will aproach that of a "flate plate" as the angle on incidence approaches 90 deg. the lift will also approach that of a flat plate as the angle of incidence approaches 90 deg.
This again is for 10 ft sq of surface. To give you the enormity of this, a neon sxt wing has an area of rougly 1.75 ft sq.
I do belive that this subject has been beaten senseless, i do not want to get into some kind of internet pissing match. im am not trying to discredit anyone or anything, just having an indepth discussion.
i strongly encourage anyone to do research on there own and not just take my word on it.
Edit: there is also a difference between power, power required, power avalable, torque, and other "forces" that are experianced by a car.