16. Jump conditions#
Starting from integral equations
\[\begin{split}\begin{aligned}
& \dfrac{d}{dt} \int_{v_t} \rho + \oint_{\partial v_t} \rho \mathbf{u}^{rel} \cdot \hat{\mathbf{n}} = 0 \\
& \dfrac{d}{dt} \int_{v_t} \rho \mathbf{u} + \oint_{\partial v_t} \rho \mathbf{u} \mathbf{u}^{rel} \cdot \hat{\mathbf{n}} = \int_{v_t} \rho \mathbf{g} + \oint_{\partial v_t} \mathbf{t}_{\mathbf{n}} \\
& \dfrac{d}{dt} \int_{v_t} \rho e^t + \oint_{\partial v_t} \rho e^t \mathbf{u}^{rel} \cdot \hat{\mathbf{n}} = \int_{v_t} \rho \mathbf{g} \cdot \mathbf{u} + \oint_{\partial v_t} \mathbf{t}_{\mathbf{n}} \cdot \mathbf{u} - \oint_{\partial v_t} \mathbf{q} \cdot \hat{\mathbf{n}} \\
\end{aligned}\end{split}\]
and collapsing the volume \(v_t\) on one of its dimension, volume contributions become negligible when compared to surface contributions. Jump conditions immeadiately follow, setting \(\hat{\mathbf{n}} = \hat{\mathbf{n}}_2 = - \hat{\mathbf{n}}_1\),
\[\begin{split}\begin{aligned}
0 & = [ \rho u^{rel}_n ] \\
\mathbf{0} & = [ \rho \mathbf{u} u^{rel}_n - \mathbf{t}_{\mathbf{n}} ] \\
0 & = [ \rho e^t u^{rel}_n + \mathbf{t}_{\mathbf{n}} \cdot \mathbf{u} - \hat{\mathbf{n}} \cdot \mathbf{q} ] \\
\end{aligned}\end{split}\]
Thus \(\rho_1 u_{n,1}^{rel} = \rho_2 u_{n,2}^{rel} = \dot{m}\), and
\[\begin{split}\begin{aligned}
0 & = [ \rho u^{rel}_n ] \\
\mathbf{0} & = \dot{m}[ \mathbf{u} ] - [ \mathbf{t}_{\mathbf{n}} ] \\
0 & = \dot{m}[ e^t ] + [ \mathbf{t}_{\mathbf{n}} \cdot \mathbf{u} - \hat{\mathbf{n}} \cdot \mathbf{q} ] \\
\end{aligned}\end{split}\]
If viscous streass and conduction heat flux are negligible,
\[\begin{split}\begin{aligned}
0 & = [ \rho u^{rel}_n ] \\
\mathbf{0} & = \dot{m}[ \mathbf{u} ] + [ p \mathbf{n} ] \\
0 & = \dot{m}[ e^t ] + [ p \hat{\mathbf{n}} \cdot \mathbf{u} ] = \\
& = \dot{m}[ e^t ] + \left[ \frac{p}{\rho} \underbrace{\hat{\mathbf{n}} \cdot \rho ( \mathbf{u} - \mathbf{u}_s )}_{ \rho u_{n}^{rel} = \dot{m}} + p \hat{\mathbf{n}} \cdot \mathbf{u}_s \right] = \\
& = \dot{m} \left[ e^t + \frac{p}{\rho} \right] + [ p \hat{\mathbf{n}} \cdot \mathbf{u}_s ] = \\
& = \dot{m} \left[ h^t \right] + \left[ p \right] \, \hat{\mathbf{n}} \cdot \mathbf{u}_s \\
\end{aligned}\end{split}\]
Two main cases are determined by the value of the mass flow \(\dot{m}\):
if \(\dot{m} = 0\),
\[\begin{split}\begin{aligned} & \dot{m} = 0 \\ & [ p ] = 0 \ , \end{aligned}\end{split}\]while nothing can be said about the tangential component of the velocity field and the total enthalpy
if \(\dot{m} \ne 0\)
\[\begin{split}\begin{aligned} 0 & = [ \dot{m} ] = [ \rho u_{n}^{rel} ] \\ \mathbf{0} & = \dot{m} [ \mathbf{u}_{\mathbf{t}} ] \\ 0 & = \dot{m} [ u_n ] + [ \, p \, ] \\ 0 & = \dot{m} [ h^t ] + u_{s,n} [ \, p \, ] = \\ & = \dot{m} \left[ h^t \right] - u_{s,n} \, \dot{m} \left[ u_n \right] = \\ & = \dot{m} \left[ h + \frac{u_n^2 + u_t^2}{2} - u_{s,n} u_n \right] = \\ & = \dot{m} \left[ h + \frac{u_n^2 - 2 u_{s,n} u_n + u_{s,n}^2}{2} - \frac{u_{s,n}^2}{2} + \frac{u_t^2}{2} \right] = \\ & = \dot{m} \left[ h + \frac{(u_n - u_{s,n})^2}{2} - \frac{u_{s,n}^2}{2} + \frac{u_t^2}{2} \right] = \\ & = \dot{m} \left[ h^{t,rel} \right] \ , \end{aligned}\end{split}\]as \(\left[ u_{s,n}^2 \right] = 0\), and with the definition of the relative total enthalpy
\[h^{t,rel} := h + \frac{1}{2} \left( (u_n - u_{s,n})^2 + u_t^2 \right) = h + \frac{1}{2} \left( \left( u_{n}^{rel} \right)^2 + u_t^2 \right) \ . \]