Air flowing at (40 mathrm{kPa}, 265 mathrm{~K}), and (mathrm{Ma}_{1}=2.0) is forced to undergo a compression turn of

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Air flowing at \(40 \mathrm{kPa}, 265 \mathrm{~K}\), and \(\mathrm{Ma}_{1}=2.0\) is forced to undergo a compression turn of \(15^{\circ}\). Determine the Mach number, pressure, and temperature of the air after the compression.

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