Stationary Normal Shock
fullflow.StationaryNormalShock
Stationary normal shock model for ideal-gas flow.
StationaryNormalShock computes downstream Mach number and normal-shock property ratios for a stationary shock in an inertial reference frame. The component can use either upstream Mach number or static pressure ratio as the defining input.
Parameters
| Name | Type | Description |
|---|---|---|
name | str | Component name |
network | Network | Network that owns this component |
specific_ | State | Specific heat ratio |
upstream_ | State, optional | Upstream Mach number |
static_ | State, optional | Upstream-to-downstream static pressure ratio |
Outputs
| Name | Type | Description |
|---|---|---|
downstream_ | State, optional | Downstream Mach number |
static_ | State, optional | Downstream-to-upstream static temperature ratio |
density_ | State, optional | Downstream-to-upstream density ratio |
velocity_ | State, optional | Downstream-to-upstream velocity ratio |
total_ | State, optional | Downstream-to-upstream total pressure ratio |
total_ | State, optional | Downstream-to-upstream total temperature ratio |
sonic_ | State, optional | Downstream-to-upstream sonic area ratio |