A light airplane, with mass (M=1000 mathrm{~kg}), has a conventionalsection (NACA 23015) wing of planform area (A=10
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A light airplane, with mass \(M=1000 \mathrm{~kg}\), has a conventionalsection (NACA 23015) wing of planform area \(A=10 \mathrm{~m}^{2}\). Find the angle of attack of the wing for a cruising speed of \(V=63 \mathrm{~m} / \mathrm{s}\). What is the required power? Find the maximum instantaneous vertical "g force" experienced at cruising speed if the angle of attack is suddenly increased.
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Related Book For 
Fox And McDonald's Introduction To Fluid Mechanics
ISBN: 9781118912652
9th Edition
Authors: Philip J. Pritchard, John W. Mitchell
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