Is the effect of downwash angle variation affecting control surfaces in the tail ( namely the elevator ), on non FBW aircraft, modeled in AEFS2 - or possible to be modeled ?
This applies, for instance to aircraft where the effect of lowering the flaps changes the AoA of the tail dramatically, and can even exert a force in the elevator that the pilot has to counter, because otherwise the sitck will move in the cockpit - ahed, in the case of a Spitfire for instance, causing the pitching down ...
I know AEFS2 calculates downwash variations, but, could or is this already modeled ?