I had 1/2 already included from that NASA link)))Scotracer wrote:The coefficient of lift wont be calculated for an F1 car, it will be found in the wind-tunnel or CFD because it runs directly from chord length and plan area etc - something that isn't directly applicable.
Oh and I've been an eejit, it's F = 1/2*rho*A*U^2*Cl - woops![]()
The area is the plan area - the surface area that the air is subject to. 2.75 (or whatever it is after you redo it without my idiocy included) on a car that is 4.5x1.8 metres does seem a bit low but when you consider the size of the floor and the wings, it might not be too far off.
Well, Maybe 2.75 isn't too far off... The floor width is 1.4 meter I believe? With all the cut outs and length about 2 meters it should be close.