autogyro wrote:
Ah yes but you are still not confirming that reducing DF does not reduce drag.
The correct sentence would be "I didn't understand your message".
It does reduce drag and keeping the high DF levels in F1 just to suit the aero lobby prevents any other work to rectify the other factors effecting wake turbulance that you are explaining.
No it doesn't necessarily decrease drag.
If i vary the design (3rd time) with aspect ratio (which involves end plates, surface), spanwise load (3D profiles),chordwise pressure integration (2D profile) Localisation relative to freestream (x,y,z coordinates),camber, cascades (vortex generators) i can have both extremes.
How?
If you: decrease aspect ratio(small wings, no end plates),have an outer span load shape (no endplates, no 3D profile), long chord (deep wings), low profile (flat wings), no GE front wing (heightened wing) you'll have low downforce, high drag.
If you: increase aspect ratio (large wings with V or C shaped endplates), have an elliptic span load shape (end plates, twisted wing tips),short chord, high profile (2D profile with circulation optimization), GE front wing, progressive venturi channels, you'll have high downforce, low drag.
All you are doing by countering arguments to reduce DF levels is keeping the extreem and not needed expense of countless aero people being paid to quote the very figures you are quoting, to baffle everyone else and by doing so you are killing any future for F1.
Lol, stop with you paranoia. You probably don't realize that Aeros is the cheapest way to be competitive; If they were not there, gaining advantage by tyres/chassis/engine would cost 3 times more!