A diffuser is to be designed to reduce the mach number of


1. A nozzle is to be designed to accelerate the flow of air from a Mach number of 0.100 to 1.00. Determine the inlet to exit area ratio of the nozzle assuming isentropic flow.

2. A diffuser is to be designed to reduce the Mach number of air from 0.90 to 0.10. Assuming isentropic flow, determine the exit to inlet area ratio of the diffuser.

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Physics: A diffuser is to be designed to reduce the mach number of
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