How does the recovery from a stall change as the center of gravity (CG) location is moved rearward?

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Multiple Choice

How does the recovery from a stall change as the center of gravity (CG) location is moved rearward?

When the center of gravity (CG) of an aircraft is moved rearward, the aerodynamic characteristics and control effectiveness are affected in a way that makes recovery from a stall progressively more difficult. This is primarily due to changes in the aircraft's stability and control authority.

A further rearward CG location generally decreases the static stability of the aircraft, which can lead to a higher tendency to pitch up during flight. In a stall condition, the aircraft experiences a loss of lift, and effective control input becomes crucial for recovery. With a rearward CG, the control surfaces may become less effective at restoring the aircraft to a normal flight attitude, making it harder for the pilot to initiate recovery. Additionally, a rearward CG can increase the stall angle of attack, thus increasing the risk of a deeper stall condition.

As the CG moves closer to the limits of the aircraft's designed range, the risk of uncontrolled flight characteristics increases, which ultimately results in a more difficult recovery scenario from a stall. Therefore, as the CG moves rearward, the dynamic response of the aircraft becomes less stable during stall recovery, necessitating greater pilot skill and experience to return to controlled flight.

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