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Find sideslip angle if [u, v, w] = [100, 5, 2.5]. Consider steady level flight.(a) 2.86°(b) 4.5°(c) 4.7°(d) 2.1°I had been asked this question during an interview.The doubt is from Lateral-Directional Static Stability and Control topic in portion Stability, Control, and Handling Qualities of Aircraft Design |
Answer» Right answer is (a) 2.86° |
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