Properties of the flow are given at the exit plane of the two-dimensional duct shown in Figure

Question:

Properties of the flow are given at the exit plane of the two-dimensional duct shown in Figure P8.10. The receiver pressure is 12 psia.

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(a) Determine the Mach number and temperature just past the exit (after the flow has passed through the first wave formation). Assume that \(\gamma=1.4\).

(b) Make a sketch showing the flow direction, wave angles, and so on.

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Related Book For  book-img-for-question

Fundamentals Of Gas Dynamics

ISBN: 9781119481690

3rd Edition

Authors: Robert D Zucker, Oscar Biblarz

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