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Fix name and typo in Laminar Flat Plate markdown
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_tutorials/compressible_flow/Laminar_Flat_Plate.md

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@@ -6,7 +6,7 @@ for_version: 7.0.0
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revised_by: talbring
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revision_date: 2020-03-03
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revised_version: 7.0.2
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solver: Euler
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solver: Navier Stokes
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requires: SU2_CFD
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complexity: basic
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follows:
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KIND_TURB_MODEL= NONE
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```
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To compute viscous flows, the Navier-Stokes governing equations are selected. The option `NAVIER_STOKES` implies that we wish to solve a laminar Naviwe-Stokes problem, and therefore, we must also set `KIND_TURB_MODEL= NONE`. For turbulent flows, SU2 solves the Reynolds-averaged Navier-Stokes equations by setting `SOLVER= RANS`, and SU2 currently contains implementations of the Spalart-Allmaras model and several variants (`SA`, `SA_NEG`, etc.) and the Shear Stress Transport (`SST`) model of Menter. If this were an inviscid flow problem, the user would enter `SOLVER = EULER` for the problem type. SU2 supports other governing equations, as well, and the user is invited to review the governing equations documentation page for a description of the possible options.
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To compute viscous flows, the Navier-Stokes governing equations are selected. The option `NAVIER_STOKES` implies that we wish to solve a laminar Navier-Stokes problem, and therefore, we must also set `KIND_TURB_MODEL= NONE`. For turbulent flows, SU2 solves the Reynolds-averaged Navier-Stokes equations by setting `SOLVER= RANS`, and SU2 currently contains implementations of the Spalart-Allmaras model and several variants (`SA`, `SA_NEG`, etc.) and the Shear Stress Transport (`SST`) model of Menter. If this were an inviscid flow problem, the user would enter `SOLVER = EULER` for the problem type. SU2 supports other governing equations, as well, and the user is invited to review the governing equations documentation page for a description of the possible options.
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Defining a no-slip boundary condition for viscous walls can be accomplished in one of two ways:
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