An object is traveling at Mach 5 through still air. The stationary air temperature is 300 K. Calculate the stagnation temperature and the recovery temperature of the traveling object. Tocool down the surface of this object to 1,000 K, heat must be removed Estimate a reference temperature for computing thermophysical properties. Write an equation that relates the heat flux to heat transfer coefficient and write appropriate relations for the computation of the heat transfer coefficient.