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 ----------------------------%