Lines Matching refs:flux

48 where the flux and the source terms, respectively, are given by
70 $$ (eq-ns-flux)
208 …riational form can be readily expressed by differentiating $\bm F_{\text{adv}}$ of {eq}`eq-ns-flux`
298 The flux Jacobian $\frac{\partial \bm F_{\text{adv}}}{\partial \bm q} \cdot \hat{\bm n}_i$ in each …
299 The complete set of eigenvalues of the Euler flux Jacobian in direction $i$ are (e.g., {cite}`toro2…
534 …We have solved {eq}`eq-advection` applying zero energy density $E$, and no-flux for $\bm{u}$ on th…
642 … at the top and bottom boundaries $(y = \pm 4.5)$ (zero normal velocity component, zero heat-flux).
643 The cylinder wall is an adiabatic (no heat flux) no-slip boundary condition.
671 …used no-slip and non-penetration boundary conditions for $\bm{u}$, and no-flux for mass and energy…
697 pressure is used for pressure in the inviscid flux terms (all other inviscid
698 flux terms use interior solution values). The wall is a no-slip,
699 no-penetration, no-heat flux condition. The top of the domain is treated as an