Question: There is steady flow through a converging - diverging nozzle. Outside the nozzle exit is a vacuum.a . Is the exiting flow subsonic, supersonic, or

There is steady flow through a converging-diverging nozzle. Outside the nozzle exit is a vacuum.a. Is the exiting flow subsonic, supersonic, or sonic? b. If appropriate, where would the flow be sonic? c. If the gas is argon (gamma=5/3), what is the static temperature and static pressure in terms of the stagnation conditions at the sonic point?

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