PPRuNe Forums - View Single Post - Blackburn Buccaneer - Aerodynamic parameters/Flight Test results
Old 8th Apr 2016, 10:50
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Genghis the Engineer
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In case the reason for my question wasn't obvious - if you have faith in your AoA indications, and know stalling AoA as well as CL.max, then you have dCl/Dalpha - at least if you assume linearity which should be true for most of the way from zero alpha/zero lift (if that is the case) to the stall.

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