jjn9128 wrote: ↑03 Aug 2018, 10:07
M840TR wrote: ↑03 Aug 2018, 06:59
The final simplification appears to be a limit on the number of elements allowed in the front wing volume - a rule already enforced for the rear wing. The number of elements is not a means of generating more downforce, but will instead affect how the wing behaves as it moves closer or further from the ground. The low position of the front wing means it's ground clearance is significantly altered by small changes in ride height, which can stall the front wing when the car pitches forwards under braking - when the car needs front grip the most. This could lead to a lower rake (flatter attitude) philosophy than pioneered by Red Bull and copied by most teams on the grid in the last few years - to move the front wing further from the ground.
How does the number of elements (I'm guessing flaps) manipulate the wing behavior in relation to the distance from ground? Or is it the height that's being reduced?
A very simple description of a wing with a flap is it allows the lower surface to be worked harder before stalling. There are a number of mechanisms at work but the simplest is that it jets some high velocity air into a region where the air attached to the surface is starting to lose momentum - and could possibly separate. The way a front wing is different to a conventional wing is that it is so close to the ground, so the air underneath is accelerated by the proximity to the ground - as the car pitches forward under braking the front wing gets closer - as it squats under acceleration the front wing gets higher. This can significantly alter the speed of the air flowing under the wing - such that you get huge changes in pressure - where you get a spike of low pressure you get something called an adverse pressure gradient. The adverse pressure gradient is where you can get flow separating - so if you jet high speed air (low pressure) into the adverse pressure gradient and you reduce the likelihood of the flow separating. Ergo 9 element front wings.
I just want to expand on this point by jjn and actually tell you the physics going on in a little more detail.
Firstly, there are 5 effects in play here:
Slat Effect
In the vicinity of the leading edge of a flap element, the velocities due to the circulation on a main element run counter to the velocities on the flap element and so reduce pressure peaks on the downstream element. Essentially, pressure recovery is reduced and so higher angles of attack can be run because it acts to slow the velocity over the nose of the flap element
Circulation Effect
In turn, the flap element causes the trailing edge of the main element to be in a region of high velocity that is inclined to the average line at the rear of the main element.
Such flow inclination induces considerably greater circulation on the main element. The trailing edge is effectively at a higher angle of attack due to the "turning" of the flow in that local region.
Dumping Effect
Because the trailing edge of the maiun element is in a region of velocity which is appreciably higher than the freestream velocity, the boundary layer on the main element "dumps" off the surface at a high velocity.
This relieves the pressure rise impressed on the boundary layer which helps to reduce the chance of separation problems occuring.
Not only does the "Circulation Effect" occur, the tangential velocity at that point is also increased by the flap element. More load can therefore be sustained without increasing the likelihood of stalling the wing.
Off-The-Surface Pressure Recovery
The boundary layer from the forward elements is "dumped" at velocities which are appreciably higher than the freestream around it. Because of this, the final decelleration back to whatever the freestream velocity is, happens in a more efficient manner because the wake region is reverting out of contact with any aerodynamic surface. This is more efficient than the best possible recovery when you are in contact with a wall.
Fresh Boundary Layer Effect
Each new element starts out with a fresh boundary layer at it's leading edge. And so because of this, the boundary layer is effectively kept "thinner" for a larger proportion of the total distance of your wing assembly. Thin boundary layers are more able to withstand adverse pressure gradients, which again, helps with pressure recovery and minimizing the chances of flow separation.
Those are the 5 main effects present when you add a flap to an aerofoil, and I will say again that pressure recovery is much more efficient in the wake region than on/in the attached boundary layer. So it is beneficial to increase the velocity at the trailing edges of an element as much as possible.
In summary,
The finite suction at the trailing edge of the main element results in a less severe pressure recovery from the suction peak (damping effect). Large regions of separated flow can be seen when you incline a single element to a similar position as the flap element is. For double-element wings, separation is not as widespread and the main element produces more downforce due to the presence of the flap element (circulation effect).
For the majority of cases, the flow remains attached to teh trailing edge of the main element. The increase in downforce as the ground is moved closer to is significantly smaller for the flap element than the main element due to being located at a higher position than the main one.
As the height of the wing is changed, the flap is farther from the ground and therefore less sensitive to changes in ride height than the main element.
There is a more significant reduction in downforce at the lowest height for a high flap angle, which is caused by the boundary layer separating over the flap. The lower circulation imparted by the flap on the main element can be seen as represented by the lower suction on the main element suction-surface for the lowest height.
This has turned into a bit of a longer post than I thought... I pulled out my "CFD Bible" and found some of my additional notes on this topic
Hope it helps, and any questions, please do ask.