Concept:
Throttling is a steady-flow expansion process across a restriction (such as a valve or porous plug) characterized by negligible heat transfer, no external shaft work, and negligible changes in kinetic and potential energies. Consequently, it is a constant enthalpy (isenthalpic) process ($h_1 = h_2$).
The behavior of temperature relative to pressure changes during this expansion is defined by the Joule-Thomson coefficient ($\mu_{JT}$):
\[
\mu_{JT} = \left(\frac{\partial T}{\partial P}\right)_h \approx \frac{\Delta T}{\Delta P} = \frac{T_2 - T_1}{P_2 - P_1}
\]
Where:
• $\mu_{JT} > 0$ implies cooling occurs during expansion ($\Delta P < 0 \rightarrow \Delta T < 0$).
• $\mu_{JT} < 0$ implies heating occurs during expansion ($\Delta P < 0 \rightarrow \Delta T > 0$).
Step 1: Gather and list the given state properties.
The parameters specified in the problem statement are:
• Initial Pressure, \(P_1 = 50 \text{ bar}\)
• Final Pressure, \(P_2 = 10 \text{ bar}\)
• Initial Temperature, \(T_1 = 300 \text{ K}\)
• Joule-Thomson coefficient, \(\mu_{JT} = -0.05 \text{ K/bar}\)
Step 2: Compute the change in pressure (\(\Delta P\)).
The pressure difference experienced by the real gas during this throttling expansion is:
\[
\Delta P = P_2 - P_1 = 10 \text{ bar} - 50 \text{ bar} = -40 \text{ bar}
\]
Step 3: Relate the parameters to find the final exit temperature (\(T_2\)).
Using the finite difference approximation for the Joule-Thomson relation:
\[
T_2 - T_1 = \mu_{JT} \times \Delta P
\]
Substituting the known values into the algebraic equation:
\[
T_2 - 300 = (-0.05 \text{ K/bar}) \times (-40 \text{ bar})
\]
Multiplying the two negative numbers together produces a positive value:
\[
T_2 - 300 = 2 \text{ K}
\]
Isolating $T_2$ by moving 300 to the right-hand side:
\[
T_2 = 300 + 2 = 302 \text{ K}
\]
Because the Joule-Thomson coefficient is negative, the gas undergoes heating during expansion, raising its temperature to approximately 302 K, which corresponds to Option (B).