Determine the exit to inlet area ratio of the diffuser

Reference no: EM131347057

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.

Reference no: EM131347057

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