A blunt-nosed aerodynamic model is mounted in the test section of a supersonic wind tunnel. If the
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A blunt-nosed aerodynamic model is mounted in the test section of a supersonic wind tunnel. If the tunnel reservoir pressure and temperature are \(10 \mathrm{~atm}\) and \(800^{\circ} \mathrm{R}\), respectively, and the exit-to-throat area ratio is 25 , calculate the pressure and temperature at the nose of the model.
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Gabriela Rosalía Castro
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