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Which increased flight control instability results when an aircraft experiences flutter?

A)Aeroelastic instability self-excites oscillations
B)Compressible flow induces shock stalling
C)Boundary layer grows uncontrollably early
D)Turbulence overwhelms control surface actuators

💡 Explanation

Destructive flutter creates dangerous oscillations because aeroelastic instability, involving aerodynamic forces and structural elasticity, amplifies them. Therefore, self-excited aeroelastic divergence causes structural failure rather than just compressibility effects or normal turbulent aerodynamic load.

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