In a problem similar to Problem 8.2, (theta_{1}) is unknown, but (theta_{2}=15.90^{circ}) and (theta_{3}=82.25^{circ}). Can you determine
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In a problem similar to Problem 8.2, \(\theta_{1}\) is unknown, but \(\theta_{2}=15.90^{\circ}\) and \(\theta_{3}=82.25^{\circ}\). Can you determine the initial Mach number?
Data in Problem 8.2,
A Schleiren photo of the flow around a corner reveals the edges of the expansion fan to be indicated by the angles shown in Figure P8.2. Assume that \(\gamma=1.4\).
(a) Determine the Mach number before and after the corner.
(b) Through what angle was the flow turned, and what is the angle of the expansion fan \(\left(\theta_{3}\right)\) ?
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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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