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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Textbook Question
Chapter 9, Problem 115P
A wing model of 5 in. chord and 2.5 ft span is tested at a certain angle of attack in a wind tunnel at 60 mph using air at 14.5 psia and 70° F. The lift and drag are found to be 6.0 lbf and 0.4 lbf respectively. Calculate the lift and drag coefficient for the model at this angle of attack.
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Chapter 9 Solutions
Fox and McDonald's Introduction to Fluid Mechanics
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