Fox and McDonald's Introduction to Fluid Mechanics
9th Edition
ISBN: 9781118912652
Author: Philip J. Pritchard, John W. Mitchell
Publisher: WILEY
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Chapter 9, Problem 120P
The NACA 23015 airfoil is to move at 180 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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Chapter 9 Solutions
Fox and McDonald's Introduction to Fluid Mechanics
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