Air enters a constant area duct at a Mach number, pressure, and temperature of M1 = 3, P1 = 1.2 atm, and T1 = 300 K, respectively. Inside the duct, the heat added per unit mass is 3 * 105 J/ kg. Calculate the flow propertiesM2, P2, T2, To2, and po2 at the exit of the duct. Assume Cp =1005 J/kg K.Use the following governing equations for flow with heat added: 1+yM (1) 1+yM P2 PI 1+yM T2 (2) huren ) Cant Poz Po = 1+yM 1+yM (3) 1+ L M 1+yM TO TO - ()()() ? 1+"M} 1+ L M (4) TO = 1 + xz+M2 (5) and 9 To, To, = (6) Properties at the exit of the duct: Mach number = 2.12](Round the answer to two decimal places.) Pressure = 3.631 atm (Round the answer to three decimal places.) Temperature = 599 K (Round the answer to the nearest whole number.) Total temperature = 1139 K (Round the answer to the nearest whole number.) Total pressure 9.96 atm (Round the answer to two decimal places.)