Standard atmospheric air [T0 = 288 K, p0 = 101 kPa(abs)] is drawn steadily through an isentropic converging nozzle into a frictionless diabatic (q = 500 kJ/kg) constant area duct. For maximum flow, determine the values of static temperature, static pressure, stagnation temperature, stagnation pressure, and flow velocity at the inlet [section (1)] and exit [section (2)] of the constant area duct. Sketch a temperature-entropy diagram for this flow.