Recognizing that the Mach waves emanating from the curved wall eventually coalesce into an oblique shock that

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Recognizing that the Mach waves emanating from the curved wall eventually coalesce into an oblique shock that turns the flow in the far field. What additional structure(s) must form at the coalescence point? Support your reasoning by calculating the Mach number and pressure downstream of the coalescence point.

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Fundamentals Of Aerodynamics ISE

ISBN: 9781266076442

7th Edition

Authors: John D. Anderson, Jr, Christopher P Cadou

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