(adsbygoogle = window.adsbygoogle || []).push({}); 1. The problem statement, all variables and given/known data

Given To/To* relationship find the associated Mach value.

2. Relevant equations

To/To=(2*(g+1)*M^2)/((1+g*M^2)^2)*(1+(g-1)/2*M^2)

where g=ratio of specific heat (gamma)

3. The attempt at a solution

I tried using matlab to plot To/To* as a function of M but I need to be able to find M as a function of To/To*

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# Rayleigh Flow

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