[NSRCA-discussion] Snap Entry

[Nat Penton]

The lead wing is seeing a rapidly increasing angle of attack due to  elevator input. When the aileron initiates this exceeds the stall angle of attack for the lead wing. The lagging wing is seeing a reduced angle of attack and does not stall.

Stall is independent of speed and dependent on angle of attack.

Inputs for all three axis can be initiated simultaneously.
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