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An aircraft experiences sideslip of 4° and side wash at vertical tail is 1.2°. What will be the AOA at vertical tail?(a) 5.2°(b) 6.89°(c) 1.2°(d) 21.3°I had been asked this question in an online interview.My query is from Lateral-Directional Static Stability and Control topic in chapter Stability, Control, and Handling Qualities of Aircraft Design |
Answer» CORRECT answer is (a) 5.2° For explanation I would SAY: AOA = SIDESLIP + SIDE WASH = 4°+1.2° = 5.2°. |
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