Greetings!
Thanx very much for the reply. I will try to look for the books. I guess i ll take the first approach bcos drag should can be reduced at further design stage, down force is much important in my case. Btw, i have been searching around in internet, is there any links to airfoil profile catalogue?
(the points, Cd, CL, Naca series etc...)
Thanks again. This forum is very knowledgable.
Monstrobolaxa wrote:"competition car downforce" - Simon Mcbeath
Like Simon points ou in his book on a first simplistic approach though you have 2 alternatives!
First - figure out the amount of downforce you want (don't look at drag now)...grab the wing width you want....through a simplistic calc you can figure out the CL of the wing.....then grab a airfoil profile catalogue and take a look at the profiles there....and choose the one that best suits you.
Second - if you have the the Hp of the engine...you can determine the amount of Hp you're willing to sacrifise for drag (hp at the wheels not at the flywheel...so consider the losses)...with this info you can calculate the Cd of the wing.....and going to the catalogue once again.....
You can also include the weight distribuition in order to know what the diference of downforce is between the front and back to maintain an aproximatly the same amount of diference between downforce at the front and rear, and weight dist front-rear.
After this I'd say.....go to a 3D design software....and after that start CFD testing....untill you find reasonable/expected values! Then tweek with the wing shape...position....kinds of profiles.
The first approach actually is my own approach (didn't read it)....the second one came from the book! I prefer to start with the downforce even if it compromises drag and then try to eliminate drag....