Generate the one dimensional normal shock functions

Reference no: EM131036219

Repeat Prob. 17-143 for methane with k =1.3.

Prob. 17-143

Using EES (or other) software and the relations given in Table A-33, generate the one dimensional normal shock functions by varying the upstream Mach number from 1 to 10 in increments of 0.5 for air with k =1.4.

Reference no: EM131036219

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