In Prob. 938 we developed expressions for u, v, and r for flow through the compressible

Chapter 9, Problem 9-73

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In Prob. 938 we developed expressions for u, v, and r for flow through the compressible, twodimensional, diverging duct of a high-speed wind tunnel. Generate an expression for the compressible stream function cr that describes this flow field. For consistency, set cr 5 0 along the x-axis. Plot several streamlines and verify that they agree with those you plotted in Prob. 938. What is the value of cr at the top wall of the diverging duct?

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