1.

Determine the value of rudder deflection r for an aircraft which is flying in north with the velocity of 60.5 m/s under the crosswind of 5m/s from east to west with Cn =0.02/deg and Cn r = -0.045/deg, where sideslip angle is -4.72 .

A. -2.09
B. 3.5
C. -4.5
D. -4.74
Answer» B. 3.5


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