Reconsider Prob. 1785E. Using EES (or other) software,
Chapter 17, Problem 1786E(choose chapter or problem)
Reconsider Prob. 1785E. 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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