Fundamentals of Aerodynamics
Fundamentals of Aerodynamics
6th Edition
ISBN: 9781259129919
Author: John D. Anderson Jr.
Publisher: McGraw-Hill Education
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Chapter 9, Problem 9.14P

Consider a diamond-wedge airfoil such as shown in Figure 9.36, with a half-angle ε = 10 ° . The airfoil is at an angle of attack α = 15 ° to a Mach 3 freestream. Calculate the lift and wave-drag coefficients for the airfoil.

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