astracrazy wrote:i'm really confused with all this suction stuff etc. with the rear wing
please can some1 explain it simply for me what the theory is?
Thanks and sorry for sounding dumb
Not dumb, perfectly valid question.
So, a wing has, in general, a long curved upper surface and a shorter lower surface (you also get symmetric profiles that are the same top and bottom, but don't worry about that for the mo).
Essentially, packets of fluid that are in contact at the front or leading edge of the wing will be in contact at the back or trailing edge. For this to happen, the flow over the top must travel faster than the flow over the bottom as the top surface is longer.
EDIT: It has been pointed out to me by a later poster that this is in fact the "equal transit-time fallacy". The fluid packets need not meet again at the end of the wing, and most likely won't. In reality, a phenomenon known as circulation is set up about a wing which causes the differential in velocity top and bottom. Lift via circulation can be witnessed when you kick a football and it swerves, for instance. On a wing, the circulation is set up by the shape and angle of attack of the aerofoil and then maintained by the necessity for equal pressure at the sharp trailing edge of the aerofoil. If you removed the external flow from a lifting aerofoil you would see that the remaining velocity travels in clockwise circles about the foil (if the oncoming flow is left to right). Still, personally, I quite like the "equal transit-time fallacy" as a pointer towards circulation theory.
This difference in speed generates a low pressure on the top (suction side) and a high pressure on the bottom (pressure side). This difference in pressure causes the wing to generate lift. Reverse it for a F1 car and you get DF.
Now, the steeper the angle you place your wing relative to the oncoming flow, the higher your lift will be (and drag normally), until at a certain angle the flow attached to the suction side of the wing can no longer hold on and separates. This process simply produces more drag for no extra lift.
If high velocity flow can be injected into the flow on the suction side in the direction tangent to it, then this separation can be delayed with excellent lift benefits (a bit like having an extra wing).
What is odd is that (as far as I can tell) all blown flaps are normally driven by a pump (normally an aircraft engine), yet these F1 versions would be seem to be passive. This is what concerns me about sharing the engine snorkel as the deficit for using the flow from there to blow the slot is likely to manifest itself here as some sort of back pressure. I should imagine it's quite a delicate system which is maybe why the slot size has changed.
Anyway, that's my ten pence worth. Hope that explains the semantics a little better.