Fundamentals of Aerodynamics
Fundamentals of Aerodynamics
6th Edition
ISBN: 9781259129919
Author: John D. Anderson Jr.
Publisher: McGraw-Hill Education
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Chapter 2, Problem 2.7P

The velocity field given in Problem 2.3 is called source flow, which will be discussed in Chapter 3. For source flow, calculate:

a. The time rate of change of the volume of a fluid element per unit volume.

b. The vorticity.

Hint: It is simpler to convert the velocity components to polar coordinates and deal with a polar coordinate system.

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