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Originally Posted by FG28_Kodiak
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Do you have any information who compiled and printed this, and where was it published? I guess it is a translation of an official document? Just being curious.
Anyway, what LtBear is asking for is just not obtainable. I tried to do this for a plane I am working on, whose flight characteristics are unknown due to lack of flight test data, and the result is just not verifiable...
I used the Theory of wing sections (Anderson) for computation of lift, and I ended up with some values which were overestimating the critical AoA of this aircraft (based on similar aircraft and their AoAcrit in IL-2) by 3-4 degrees.
Anyway, in order to do this, you have to have a complete understanding of how the FM is represented in this simulation, and when I say "complete" I mean complete as in the case of its creator, if you get my drift.