Castor angle is defined as the angle

A Formed by the longitudinal axis of the aircraft and the direction of movement of the nose gear
B Between the direction of wind and the longitudinal axis of the runway
C Between the true speed of the aircraft and the crosswind component
D Between the horizontal and the fuselage axis

Correct Answer: Formed by the longitudinal axis of the aircraft and the direction of movement of the nose gear

Bissoy MCQ
#Civil Engineering #Airport Engineering

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