Engineering - Airport Engineering - Discussion

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Q.

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

Answer: Option a
Explaination:

 


No Explanation




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