A supersonic flow at M 1 = 1.58 and P 1 = 1 atm expands around a

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A supersonic flow at M1 = 1.58 and P1 = 1 atm expands around a sharp corner. If the pressure downstream of the corner is 0.1306 atm, calculate the deflection angle of the corner.

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Managerial Accounting For Undergraduates

ISBN: 9780357499948

2nd Edition

Authors: James Wallace, Scott Hobson, Theodore Christensen

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