At a point in the flow over a high-speed missile, the local velocity and temperature are (3000
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At a point in the flow over a high-speed missile, the local velocity and temperature are \(3000 \mathrm{ft} / \mathrm{s}\) and \(500^{\circ} \mathrm{R}\), respectively. Calculate the Mach number \(M\) and the characteristic Mach number \(M^{*}\) at this point.
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