Vyssion wrote: ↑18 Aug 2017, 13:02
jjn9128 wrote: ↑18 Aug 2017, 11:50
PlatinumZealot wrote: ↑18 Aug 2017, 00:53
Too early, too early. Those equations are not pretty either. But in layman's terms for a given momentum as the pressure differential across the surface ( dp/dx) increases the boundary layer thickness is less. So simply put, having the fan reduces energy loss under the floor - that energy saved, you can use it for less drag or more downforce up to you.
I would also be interested in seeing a proof or at least a schematic of how it works/feeds into the undertray.
The drag of an F1 car is dominated by induced drag, not just from downforce but sideforce too. In fact viscous drag is a tiny part of overall drag - I can't see active aerodynamics as a means of reducing drag within the current spec like you suggest.
^ this...
I'm curious to see what equations youre referring to as well; I have the feeling that you may be implying the opposite of one effect under one type of geometry as being the flow physics for the opposite geometry. If flow over a boundary occurs when there is a pressure decrease in the direction of flow, the fluid will accelerate and the boundary layer will become thinner (e.g. usually occurs in converging geometries), however, with a diverging geometry (e.g. a diffuser), the problem shifts from one that involves pressure inducing a boundary layer acceleration/thinning, to one of momentum. When the pressure increases in the direction of flow the situation is very different. Fluid outside the boundary layer has enough momentum to overcome this pressure which is trying to push it backwards. The fluid within the boundary layer has so little momentum that it will very quickly be brought to rest, and possibly reversed in direction. If this reversal occurs it lifts the boundary layer away from the surface, causing separation. I'm not sure that a fan will have enough of an impact on the momentum of the boundary layer within the diverging tunnels so as to "re-energize it" and make it thinner.
Given that the boundary layer thickness (and by extention) the coefficient of skin friction of a body is related to the Reynolds Number of the system, the fact that Re is a function of velocity means that at the surface, your local Re will be zero and thus you will not be able to totally eliminate the boundary layer. Given such a short distance that the diffusers cover at the moment, Im not sure whether the "increase" in velocity that a fan could impart to the air flow in there when the air is already travelling at ~300km/hr etc, would do enough to make a noticable difference in the thickness of the boundary layer. You also have the issue at the moment where teams employ a concave diffuser in order to rapidly increase the cross sectional area of the diffuser at the expense of generating a permanent separation bubble; there is still a net positive, and so again, I am not sure of how that solution would compare to forcing the boundary layer to remain attached and using some sort of a "sucking" fan instead.
Most F1 cars aren't struggling for downforce at 300kph+, quite opposite in fact, they want to shed downforce/induced drag at that speed, as they have more than enough downforce to navigate turns at those speeds save for at most three turns on any given track. Where F1 cars struggle at, the biggest performance difference in terms of aero comes in the low and mid speed corners. The speed range of 120-260kph is where good aero makes a difference for the vast majority of tracks, and conditions. Given the same engine, improving downforce in this speed range will make a bigger difference than downforce above it.
Aside from Copse in Silverstone, turn 11 in Hungary, Pouhon in Spa, turns 3 & 9 in Barcelona, Turn 11 & 12 in Australia, Turn 7 in China, turn 1 in Japan, and turns 5, 6 & 12 in Sepang there are no real corners in the 260kph+ speed range.