Flow in a gas turbine combustor is modeled as steady, one-dimensional, frictionless
heating of air in a channel of constant area. For a certain process, the inlet conditions
are 960°F, 225 psia, and M = 0.4. Calculate the maximum possible heat
addition. Find all fluid properties at the outlet section and the reduction in stagnation
pressure. Show the process path on a Ts diagram, indicating ail static and stagnation
state points.