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An aircraft is flying in the north direction at a velocity of 60.5m/s under cross wind from the east to west of 5m/s. If the value of Cnβ=0.02/deg, where. Find sideslip angle β.(a) -4.72°(b) -5°(c) 4.7°(d) 3.18°I had been asked this question by my school teacher while I was bunking the class.My enquiry is from Lateral-Directional Static Stability and Control in portion Stability, Control, and Handling Qualities of Aircraft Design |
Answer» The correct choice is (a) -4.72° |
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