Andy Ross wrote:
>> But before testing it with any YASim aircraft: I probably found
>> another bug in surface.cpp. For "general lift" and "flap-lift" the
>> effect of stall is calculated in stallFunc() resp FlapLift().
>
> Yup, that looks correct to me. Applied. I'm not sure what the points
> was of the extra 1.0 in the return value; maybe a holdover from an
> earlier version where this function returned a scalar coefficient, and
> not a force?
This might be a typical case where someone wanted to avoid
division-by-zero cases ;-)
Martin.
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