The NACA 23015 airfoil is to move at (180 mathrm{mph}) through standard sea level air. Determine the
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The NACA 23015 airfoil is to move at \(180 \mathrm{mph}\) through standard sea level air. Determine the minimum drag, drag at optimum \(L / D\) and drag at point of maximum lift. Calculate the lift at these points and the power that must be expended to obtain these lifts.
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Fox And McDonald's Introduction To Fluid Mechanics
ISBN: 9781118912652
9th Edition
Authors: Philip J. Pritchard, John W. Mitchell
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