A two dimensional oblique shock diffuser operates in a supersonic stream of air at an angle of
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A two dimensional oblique shock diffuser operates in a supersonic stream of air at an angle of attack 5o as shown in the figure below. If P1=101.3 kPa and M1=2.3 determine the pressures, the Mach numbers, and the direction of flow in regions 3 and 5.
Related Book For
Fundamentals of Momentum, Heat and Mass Transfer
ISBN: 978-1118947463
6th edition
Authors: James Welty, Gregory L. Rorrer, David G. Foster
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