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fixed a micro mistake of stagnation p & T #12

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Nov 13, 2020
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fixed a micro mistake of stagnation p & T #12

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2 changes: 1 addition & 1 deletion _tutorials/compressible_flow/Inviscid_Bump.md
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Expand Up @@ -78,7 +78,7 @@ MARKER_OUTLET= ( outlet, 101300.0 )

The 4 different boundary markers in the computational grid must have an accompanying string name. These marker names (upper_wall, lower_wall, inlet, and outlet for this case) are each given a specific type of boundary condition in the config file. For the inlet and outlet boundary conditions, the additional flow conditions are specified directly within the configuration option.

The inlet boundary condition type is controlled by the `INLET_TYPE` option, and the total condition type is the default. The format for the total condition inlet boundary condition is (marker name, inlet stagnation pressure, inlet stagnation pressure, x-component of flow direction, y-component of flow direction, z-component of flow direction), where the final three components make up a unit flow direction vector (magnitude = 1.0). In this problem, the flow is exactly aligned with the x-direction of the coordinate system, and thus the flow direction vector is `(1.0, 0.0, 0.0)`. The outlet boundary format is (marker name, exit static pressure).
The inlet boundary condition type is controlled by the `INLET_TYPE` option, and the total condition type is the default. The format for the total condition inlet boundary condition is (marker name, inlet stagnation temperature, inlet stagnation pressure, x-component of flow direction, y-component of flow direction, z-component of flow direction), where the final three components make up a unit flow direction vector (magnitude = 1.0). In this problem, the flow is exactly aligned with the x-direction of the coordinate system, and thus the flow direction vector is `(1.0, 0.0, 0.0)`. The outlet boundary format is (marker name, exit static pressure).

```
% ------------------------ SURFACES IDENTIFICATION ----------------------------%
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