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In linear interpolation method, new airfoil is created as ____________(a) weighted average of root and tip airfoil(b) heavier than the root airfoil always(c) higher chord than root always(d) lower chord than tip alwaysI got this question in a national level competition.I want to ask this question from Configuration Layout topic in portion Configuration Layout and Loft of Aircraft Design |
Answer» Correct OPTION is (a) weighted average of root and tip airfoil |
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