From 8437b5a140997871bfa6ab56622e34f9f1138795 Mon Sep 17 00:00:00 2001 From: Wenyin Wei Date: Thu, 25 Jul 2019 09:39:09 +0800 Subject: [PATCH] fixed a micro mistake of stagnation p & T --- _tutorials/compressible_flow/Inviscid_Bump.md | 2 +- 1 file changed, 1 insertion(+), 1 deletion(-) diff --git a/_tutorials/compressible_flow/Inviscid_Bump.md b/_tutorials/compressible_flow/Inviscid_Bump.md index 43036a7f..3884dbba 100644 --- a/_tutorials/compressible_flow/Inviscid_Bump.md +++ b/_tutorials/compressible_flow/Inviscid_Bump.md @@ -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 ----------------------------%