A 5.6-liter V8 engine, with a compression ratio of Tc = 9.4:1,operates on an air standard Otto cycle at 2800 RPM, with a volumetric efficiency l1v = 90% and a stoichiometric air-fuel ratio using gasoline. The exhaust gas flow undergoes a temperature drop of 44°C as it passes through the turbine of the turbocharger.
Calculate: (a) Mass flow rate of exhaust gas. [kg/see]
(b) Power available to drive the turbocharger compressor. [kW]