Aerospace Engineering > GATE 2016 > Aircraft Control
An aircraft is flying level in the North direction at a velocity of 55 m/s under cross wind from East to West of 5 m/s. For the given aircraft Cnp=0.012/deg and Cnδr=-0.0072/deg, where δr is the rudder deflection and is the side slip angle. The rudder deflection exerted by pilot is _______ degrees.
Correct : 8.6:8.7
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