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.
(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
Fundamentals Of Gas Dynamics
ISBN: 9781119481690
3rd Edition
Authors: Robert D Zucker, Oscar Biblarz
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