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Working from first principles, derive an expression for the nozzle exit velocity for an ideal ramjet...

Working from first principles, derive an expression for the nozzle exit velocity for an ideal ramjet in terms of: the flight velocity; the peak-post-combustor stagnation temperature; the ambient stagnation temperature. State any assumptions you use.

Please show working out and describe what is done

Derive formula in terms of respective paraneters

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