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Forum: Tech Log
10th Jun 2017, 23:31
Replies: 7
Views: 9,138
Posted By Sidestick_n_Rudder

At high Mach number, increase of the AoA...

At high Mach number, increase of the AoA intensifies the shock wave in the wing, which in turn causes flow separation and buffet. This occurs at significantly lower AoA, than classic low speed stall...
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