Mazdaboy wrote:I think they're tested the double DRS Look at the rear wing endplate. It's so much wider.
Agreed, no room for intake hole.Huntresa wrote: You do realize there is no space for a hole? I mean where the hole should be there is fins.
beelsebob wrote:The hole could be placed on the main plane of the wing, behind the DRS flap. Though I doubt it is.
New wheelnut design???Mazdaboy wrote:I think they're tested the double DRS Look at the rear wing endplate. It's so much wider.
Either that, or they are gurneys? Can't really tell. Would it be possible that it is one slot that come back on itself, from the edge of the diffuser?cccag wrote:looks like slots here ....the tarmac is visible
http://www.formule1.nl/media/uploads/me ... 040.66.jpg
Yes they're gurneys what looks like gravel through a slot is rain drops in front of the gurney I reckon.SiLo wrote: Either that, or they are gurneys? Can't really tell. Would it be possible that it is one slot that come back on itself, from the edge of the diffuser?
IANAA, but... my bet would be that the luvres encourage the air flow out of the side of the wing to be upwards, and create an extension of the wing to the sides, wheras if you had no end plate air would spill off the high preasure side of the wing sideways (rather than upwards and sideways).hardingfv32 wrote:Why bother with with the end plate above the main element? Is it requiered by the rules?
Why doesn't the end plate seal the bottom of the second element/flap? I though that an end plate on the low pressure side of a wing was always a benefit.
Not a bad thought. May I assume that these louvers in all cases provide less downforce or is there a chance of a net gain ASSUMING that the AoA is the same?beelsebob wrote:my bet would be that the luvres encourage the air flow out of the side of the wing to be upwards, and create an extension of the wing to the sides, wheras if you had no end plate air would spill off the high preasure side of the wing sideways (rather than upwards and sideways).
The endplates increase the downforce produced by the wing by effectively fooling the system in to thinking the wing is longer than it is. This is because the inevitable vortex produced at the wing tip reduce the downforce of the wing. It, in effect, makes the wing behave as if it were a shorter span. The endplates reverse this effect and so mean the wing produces more of its theoretical lift. We see these on airliners too in the form of vertical wingtips.hardingfv32 wrote:Why bother with with the end plate above the main element? Is it requiered by the rules?
Why doesn't the end plate seal the bottom of the second element/flap? I though that an end plate on the low pressure side of a wing was always a benefit.
Brian
This is what Brian was referring to re the low pressure side of the wing though. The typical method of destroying the vortex is to put a vertical segment *on the low pressure side*. Hence why airliners have wing tips that point upwards.Just_a_fan wrote:The endplates increase the downforce produced by the wing by effectively fooling the system in to thinking the wing is longer than it is. This is because the inevitable vortex produced at the wing tip reduce the downforce of the wing. It, in effect, makes the wing behave as if it were a shorter span. The endplates reverse this effect and so mean the wing produces more of its theoretical lift. We see these on airliners too in the form of vertical wingtips.hardingfv32 wrote:Why bother with with the end plate above the main element? Is it requiered by the rules?
Why doesn't the end plate seal the bottom of the second element/flap? I though that an end plate on the low pressure side of a wing was always a benefit.
Brian
Unfortunately, the whole rear wing system still produces a big vortex at each end which creates big drag. So the teams use the louvres and the cut out behind the flap to reduce these large vortices. This will reduce the downforce but it improves the overall efficiency of the system. It's about efficiency. A more efficient system gives the teams more options.