racer777
New member
- Aug 11, 2002
- 2
I'm 'designing' a race car that will have what is essentially a large inverted wing section as the body,to get max downforce ( with the leading edge between the front wheels and the trailing edge between the rears.) The top and bottom surfaces will have clean air- flow. The chord will be approx 2700mm ( 9 feet ), the span will be approx 1100mm ( 43"
& the thickness approx 500 to 600mm ( 20-24"
.The 'wing' may include front leading wing slat & rear will have a seperate adjustable flap, as well as full side fences. The "working" speed range - between 50 to 120mph, drag will not be a concern,
Questions; =suggestions for airfoil profile data,soft-ware etc for a wing with such a low AR. 'lift' figure calc.
=how to calc centre of lift for front to rear balance of car - will rear 2nd flap alter this much?
=As this wing/body is operating close to the ground it will operate more like venturi tunnel setup and so what other complications / modifications to consider.
I'm a novice in the aeronautical field so any help in simple terms is greatly appreciated.
Questions; =suggestions for airfoil profile data,soft-ware etc for a wing with such a low AR. 'lift' figure calc.
=how to calc centre of lift for front to rear balance of car - will rear 2nd flap alter this much?
=As this wing/body is operating close to the ground it will operate more like venturi tunnel setup and so what other complications / modifications to consider.
I'm a novice in the aeronautical field so any help in simple terms is greatly appreciated.