A small turbine using compressed air has a power output of 100 W.
The enthalpy of the air at the inlet is 320 kJ/kg and the enthalpy at the outlet is 240 kJ/kg. Assume the process is adiabatic and the change in the kinetic energy is negligible. Compute the mass flow rate.
"\\dot m=\\frac{S_1-S_2}W=0.8~\\frac{kg}s ."
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