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Which operational problem arises when aircraft landing gear doors experience asymmetric aerodynamic loading on descent?

A)Elevated fuel consumption occurs.
B)Runway veer induces sideslip.
C)Flutter oscillation compromises stability.
D)Increased stall speed develops.

💡 Explanation

Flutter oscillation occurs due to aeroelastic instability; because aerodynamic forces couple with the gear door's structural dynamics, creating self-excited vibrations that escalate, therefore flutter arises, rather than simple drag because of the structural interaction at high speeds.

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