Write a Matlab program that returns the freestream fluid Mach number, temperature, and velocity for Mach numbers between $0$ and $5$ assuming known $($input$)$ values of stagnation pressure from the pitot probe, $\backslash$gamma of the fluid, and the static pressure and temperature of the freestream flow. For this problem, you are expected to use the equations developed in class and in the textbook. Do not use or import any tables to obtain the solution. You must use the Matlab function 'fsolve' to solve the developed nonlinear relationship for supersonic flow. Use your Matlab code to solve Anderson problems $8\mathrm{.}11$ and $8\mathrm{.}12.$ Use your Matlab code to plot the freestream Mach number vs $($p$\_(02))/($p$\_(1))$ for $1$