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Find the degree of elevator float. Consider tail AOA is 2° and CHδe= -0.005, CHɑt=-0.0052.(a) 2.08 deg(b) 4(c) 12(d) 2.119This question was addressed to me in a national level competition.I would like to ask this question from Stick-Free Stability topic in portion Stability, Control, and Handling Qualities of Aircraft Design |
Answer» The CORRECT OPTION is (a) 2.08 deg |
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