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Air is flowing in a CD nozzle with a static pressure of 400sz at the throat and exit Mach No. of 23'. Assuming an ambient

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Air is flowing in a CD nozzle with a static pressure of 400sz at the throat and exit Mach No. of 23'. Assuming an ambient pressure of llkPa, compute the chamber pressure. Also, determine whether there will be an oblique shock or an expansion wave at the exit

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