In the flow past a compression corner, the upstream Mach number and pressure are 3.5 and (1

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In the flow past a compression corner, the upstream Mach number and pressure are 3.5 and \(1 \mathrm{~atm}\), respectively. Downstream of the corner, the pressure is \(5.48 \mathrm{~atm}\). Calculate the deflection angle of the corner.

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