I have some questions. @ Crumpp
We're other contemporary aircraft also tested in this way?
It's all good and well saying the Spit did this, this and this but, how did other aircraft stack up?
Also, how exactly do you intend to model this phenomenon in CLOD?
It seems to depend on stick forces and stick forces aren't calculated in CLOD? Or are they? We all know that the controls on these aircraft stiffend significantly at high speeds, that's not accounted for either.
So really the most important point, considering where we are is, what would you expect to be done to the FM to replicate this?
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