If you just want the thermal energy of the exhaust, do what I originally said. You need to multiply the mass flow rate by the specific internal energy [kJ/kg], which is just a function of the temperature for an ideal gas (u=2.5*R*T for a diatomic gas). The temperature you should use is the exhaust temperature.
Now, on the other hand, if you are looking for the heat from combustion, you can apply the first law for an open system and find the Q=m_dot*(h_out-h_in)=m_dot*c_p*(T_out-T_in), where T_in would be the intake temperature, and T_out would be the exhaust temperature and this is likely the temperature difference russ was referring to. But it sounds like that is not what you are looking for, so just refer to my original response.