Question: Using EES (or other) software, study the effects of both air and helium flowing steadily in a nozzle when there is a normal shock at

Using EES (or other) software, study the effects of both air and helium flowing steadily in a nozzle when there is a normal shock at a Mach number in the range 2< , Ma1 <, 3.5. In addition to the required information, calculate the entropy change of the air and helium across the normal shock. Tabulate the results in a parametric table.

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