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Homework Statement
A turbine is driven by compressed air. The air enter the turbine with temperature ##T_1## and pressure ##P_1##. When the air leaves the turbine it's pressure is lowered to ##P_2##. Calculate the work done for one mol air.
The expansion of the air can be seen as reversible and adiabatic. The contribution from the airflow as the air enters/leave the turbine can be ignored. The air can be treated as a two atomic ideal gas.
Homework Equations
Adiabatic
##Tp^{\frac{1}{\gamma}-1} =## constant
First law of thermodynamics (We consider the work done by gas, not the work done on the gas)
##\Delta U = -W+Q##
Internal energy for ideal gas (one mole)
##U=C_VRT=\frac{f}{2}RT##
##C_P = \left(\frac{\partial H}{\partial T}\right)_P##
The Attempt at a Solution
I'm having trouble seeing why my solution is incorrect:
It follows that ##T_2 = T_1 \left( \frac{P_2}{P_1}\right)^{1-\frac{1}{\gamma}}##
Since adiabatic process ##Q=0## which gives
##W = U_2-U_1 = \frac{5}{2}RT_1\left[1-\left( \frac{P_2}{P_1}\right)^{1-\frac{1}{\gamma}}\right]##
Correct solution:
##H_1 = W+H_2## gives that
##W = H_1-H_2 = C_P(T_1-T_2) = \frac{7}{2}RT_1\left[ 1-\left(\frac{P_2}{P_1}\right)^{1-\frac{1}{\gamma}} \right]##