Lecture%2025_Compressible%20Flow_part2

Lecture%2025_Compressible%20Flow_part2 - 13.23: Air at 0...

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Unformatted text preview: 13.23: Air at 0 deg C is contained in a large tank on the space shuttle. A converging section with exit area 1e-3 m^2 is attached to the tank, through which air exits to space at a rate of 2 kg/s. What are the pressure in the tank, and the pressure, temperature, and speed at the exit? 13.42: Air is to be expanded through a converging-diverging nozzle by a frictionless adiabatic process, from a pressure of 1.10 MPa (abs) and a temperature of 115 deg C, to a pressure of 141 kPa (abs). Determine the throat and exit areas for a welldesigned shockless nozzle, if the mass flow rate is 2kg/s. ...
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Lecture%2025_Compressible%20Flow_part2 - 13.23: Air at 0...

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