Consider the separated curved bow shock wave in front of the two-dimensional parabolic bluff body shown in

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Consider the separated curved bow shock wave in front of the two-dimensional parabolic bluff body shown in the figure. Free flow is Mach 8. Consider the two streamlines that pass through the impact at points a and b shown in the figure. The wave angle at point a is 90° and the wave angle at point b is 60°. Calculate and compare the entropy values of streamlines a and b in the airflow after impact (relative to free flow).

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Aerodynamics

ISBN: 9789811945861

1st Edition

Authors: Peiqing Liu

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