The following formula has been suggested as an alternate to Eq. (9.86) to relate upstream Mach number

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The following formula has been suggested as an alternate to Eq. (9.86) to relate upstream Mach number to the oblique shock wave angle β and turning angle θ: Can you prove or disprove this relation? If not, try a few numerical values and compare with the results from Eq. (9.86).

The following formula has been suggested
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