1. Compressible Isentropic Flow & Critical Sonic Choking
The critical pressure ratio defining the boundary between subcritical and sonic choked flow is given by:
\[ r_c = \left( \frac{2}{k+1} \right)^{\frac{k}{k-1}} \]
Where \(k = C_p / C_v\) is the specific heat ratio. For natural gas (\(k \approx 1.30\)), \(r_c \approx 0.5457\).
2. API RP 520 Part I Mass Discharge Equations
When the actual pressure ratio \(P_2 / P_1 \le r_c\), flow is sonically choked at the throat (\(\text{Mach } 1.0\)):
\[ \dot{m}_{crit} = C_d \cdot A \cdot P_1 \sqrt{\frac{k \cdot M}{Z_1 \cdot R \cdot T_1} \left( \frac{2}{k+1} \right)^{\frac{k+1}{k-1}}} \]
3. Joule-Thomson Isenthalpic Expansion Cooling
During unheated pressure reduction across a restriction, isenthalpic expansion induces significant Joule-Thomson cooling:
\[ \Delta T_{JT} \approx \mu_{JT} \cdot (P_1 - P_2) \qquad T_2 = T_1 - \Delta T_{JT} \]