Consider an airflow inside a one-dimensional inviscid duct with inflow Mach number = 0.2, inflow static temperature and pressure equal to 300 K and 100,000 N/m2, respectively. Calculate the total temperature, Mach number, static pressure, static temperature, and total pressure at the exit of the duct if heat is added at the rate of 1,200,000 J/kg(air)