A combustion chamber consists of tubular combustor of constant area. Compressed air enters the tube at static temperature of 300 K, static pressure of 1 atm and a Mach number of 3.0. The heat added per unit mass is q = 3x105 J/kg. Approximating combustion as a heat transfer process to air and Raleigh flow, determine the following at the exit of the combustion chamber a) Toz b) M C) P2 d) T e) Find the heat added per unit mass required to choke the flow (8 points) (6 points) (5 points) (2 points) (4 points)