Raleigh wrote:JDC123 wrote:There is no such thing as a 'dirty air' car. An aerofoil will perform worse in turbulent air due to unpredictable inertia forces that cause premature flow separation from the wing surfaces. This is a scientific fact. There is absolutely no way you could design a wing to perform better in turbulent conditions as opposed to 'clean' laminar conditions.
No, but you can make a car that will perform better in dirty air vs a car that is optimized for running in clean air (not that I'm suggesting this is what Haas have done).
As a rule, the simpler the aero the less performance will be lost by running in dirty air. A plain 2 element front wing like you'd find on a GP2 car may not generate the same downforce as an F1 front wing with it's 4-6 elements and finely tuned details, but the less complex wing retains most of its performance even if you're running right behind another car.
Indeed, you could probably design a simple wing that outright outperforms an F1 front wing when the car is running in dirty air (of course a car with this wing wouldn't be as fast as the F1 car in clean air, which is why teams don't do this). This contributes to racing frequently being closer in lower formulas than in F1, it's easier to follow another car.
Different types of aero also suffer different amounts from running in dirty air. Downforce from the floor will be less affected than downforce from the wings, and the front wing suffer more than the back wing. This is why F1 cars start understeering as soon as you get close behind another car, they keep most of the rear downforce but you lose the front end.
Please stop propagating this myth. Running a more complex wing (a wing with more elements) does not mean it will be worse running in turbulent air. It is a fallacy. It can be worse but at the same time, it can be better.
What multiple elements allows a wing to do is run at higher alpha levels (angle of attack to the apparent airflow direction {due to other cars or the airflow moving over objects a wing will see an apparent airflow, I.e. Not necessarily the same direction airflow as a different area or wing on the car}). Allowing higher levels of alpha allow for much higher Cl (coefficient of lift) values at the expense of very high Cd (coefficient of drag values). Since downforce is still king, for the most part, in F1, the designers will trade the extra drag for downforce in most cases.
What really controls how the front wing operates in turbulence is down to many other variables that weren't mentioned. Some of these are:
a. The overall camber of the wing
b. The camber and shape of each element
c. The size of the slot gaps between each element, usually the larger slot gaps will mean a lower sensitivity to airflow changes but lower maximum Cl levels
d. How close the wing is run to the ground, as the front wings are partial diffusers in their operation and function as such.
e. Vortex generators, strakes and the like which help to keep flow attached to the underside of the wing.
And many more.
A 2 element wing if pushed as hard (as close to its partial or full stall region) will actually stall worse than a 4 or 5 element wing. This is because on a 2 element wing it is very easy for a partial stall region to quickly spread forward along the chord of the wing and severely degrade performance. On a more complex wing as the rear portion stalls the slot gaps help to stop the spread of the airflow stalled region from spreading. Therefore while part of the wing will still stall, it will actually lose less downforce than a 2 element wing.
When it comes to general wing or individual wing element camber, the designers can go many different roots (pun?). Variables such as how much camber is run and where along the wing the point of maximum camber is placed partially dictate the stall characteristics of a wing. Designers can choose to be more safe and go with a design that has a wider operating speed and angle (more effective for a car that consistently runs in dirty turbulent air) or for a design that has very high Cl numbers but will deliver it over a smaller range of angles. This second design philosophy will provide more peak downforce however once the wing starts stalling the stall region will spread very quickly.
So please, stop spreading this "simpler wings = more stable downforce" nonsense.
Thank you and good night.