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Which instability occurs when exceeding a jet fighter's flight envelope with an aggressively deflected rudder?

A)Adverse yaw increases uncontrollably
B)Aileron reversal becomes dominant
C)Dutch roll oscillations intensify
D)Structural flutter induces resonance

💡 Explanation

Adverse yaw increases when the rudder creates excessive yaw, inducing differential lift and intensified drag. This is due to the mechanism of aerodynamic stall progression because flow separation exceeds design limits, therefore adverse yaw dominates, rather than aileron reversal or flutter, which have separate causal factors.

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