Gridlock wrote: ↑16 Mar 2026, 22:08
Could they be playing with the definition of the "physical stop" somehow? (emphasis added), such that the 400ms rule applies to only part of the transition?
n. when commanded, switch to one of two fixed positions defined as follows:
i. a “Corner Mode” position, that conforms to a position defined in (k) and that remains
identical following any Straight-Line Mode operation to its position beforehand.
ii. a “Straight-Line Mode” position that, when compared to the Corner Mode position,
results in a decrease in incidence of FW Primary Flap and/or FW Secondary Flap.
Furthermore, except when limited by a physical stop defined in (u), the magnitude of
decrease must remain constant.
o. have a maximum transition time between the two fixed positions that does not exceed 400ms.
...
u. Physical Stops must be provided to prevent both FW Primary Flap and FW Secondary Flap from
being rotated external to RV-FW-PROFILES.
The "physical stop" in this case is more like a railway rigid buffer stop, not the wing rotation coming to a stop. The wing can only go so far, one way or the other before it hits the stop and it must go from point A (open) to point B (closed) or vice versa in less than 400ms.
One would assume that closing the wing[s] when the car is travelling faster takes more effort to overcome than when going slower.
What happens if say a piece of rubber gets stuck near the wing and takes a few ups and downs to clear, is this like the old DRS test which was only done static with a ball not passing through, like a timer and camera on the wing moving when in parc ferme, if it passes that, then it`s fine, until someone brings it up!