You signed in with another tab or window. Reload to refresh your session.You signed out in another tab or window. Reload to refresh your session.You switched accounts on another tab or window. Reload to refresh your session.Dismiss alert
**Note 2**: Updates to the velocity based on the prescribed pressure are damped in order to help with stability/convergence. The damping coefficient can be changed using the `INC_INLET_DAMPING` option (default is `0.1`).
217
219
220
+
## Supersonic Inlet Boundary Condition ##
221
+
Supersonic inlet boundary conditions are set using the option `MARKER_SUPERSONIC_INLET`.
The format for `MARKER_SUPERSONIC_INLET` for the NEMO solvers is the marker name, followed by the static translational-rotational Temperature (in Kelvin `[K]`), the static Pressure (in Pascal `[Pa]`) and the flow velocity vector (in meter per second `[m/s]`). For example:
For the NEMO solvers, a gas composition at the inlet must also be specified using the `INLET_GAS_COMPOSITION` option, as well as the vibrational-electronic Temperature at the inlet, using the `INLET_TEMPERATURE_VE` option. If no vibrational-electronic Temperature is specified, the given translational-rotational Temperature set for the inlet is used by default. For example:
0 commit comments