Question: For an optimum nozzle ( i . e . , nozzle exit pressure = ambient pressure ) , the nozzle expansion ratio ( A e

For an optimum nozzle (i.e., nozzle exit pressure = ambient pressure), the nozzle expansion ratio (AeAt) is a function of the flight altitude. Please make a plot similar to the one below for gamma =1.1 and 1.3, and discuss the effect of gamma on the nozzle expansion ratio.
For an optimum nozzle ( i . e . , nozzle exit

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