Develop a computer progran1 that, given the area ratio, ratio of specific heats, and
Chapter 12, Problem 12.47(choose chapter or problem)
Develop a computer progran1 that, given the area ratio, ratio of specific heats, and flow condition (subsonic or supersonic) as input, provides the Mach number. This will require some numerical root-finding scheme. Run the program for an area ratio of 5 and ratio of specific heats of 1.4. Compare the results with those in Table A.l. Then run the program for the same area ratio but with the ratios of specific heats of 1.67 (helium) and 1.31 (methane). This progran1 will be useful for Probs. 12.50, 12.51, and 12.54- 12.60.
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