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  3. a steady flow of air at 360 k and 02...

Question: a steady flow of air at 360 k and 02...

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2. A steady flow of air at 360 K and 0.2 MPa enters a diffuser with a Mach number of 0.8. The total pressure recovery factor is 0.95. Determine the static pressure and temperature at the exit if M 0.15 at [18 points] that section.

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