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1 change: 1 addition & 0 deletions _data/docs_v7.yml
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Expand Up @@ -40,6 +40,7 @@
- Physical-Definition
- Markers-and-BC
- Convective-Schemes
- Slope-Limiters-and-Shock-Resolution
- Custom-Output
- Linear-Solvers-and-Preconditioners
- Multizone
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1 change: 1 addition & 0 deletions _data/tutorials.yml
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- Laminar_Cylinder
- Turbulent_Flat_Plate
- Transitional_Flat_Plate
- Transitional_Flat_Plate_T3A
- Turbulent_ONERAM6
- Unsteady_NACA0012
- UQ_NACA0012
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1 change: 1 addition & 0 deletions _data/vandv.yml
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- Bump_Channel
- 30p30n
- swbli
- LM_transition
1 change: 1 addition & 0 deletions _docs_v7/Physical-Definition.md
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Expand Up @@ -21,6 +21,7 @@ SU2 offers different ways of setting and computing this definition. This documen
- [Turbulence Models](#turbulence-models)
- [Spalart-Allmaras (SA)](#spalart-allmaras-model)
- [Shear Stress Transport (SST)](#shear-stress-transport)
- [Transition Models](#transition-models)

---

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@@ -1,11 +1,8 @@
---
title: Transitional Flat Plate for T3A and T3A-
permalink: /tutorials/Transitional_Flat_Plate/
permalink: /tutorials/Transitional_Flat_Plate_T3A/
written_by: Sunoh Kang
for_version: 7.4.0
revised_by: -
revision_date: -
revised_version: -
for_version: 7.5.0
solver: RANS
requires: SU2_CFD
complexity: basic
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2 changes: 1 addition & 1 deletion _tutorials/index.md
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Expand Up @@ -40,7 +40,7 @@ Simulation of external, laminar flow around a 2D cylinder.
Simulation of external, turbulent flow over a flat plate (classical RANS validation).
* [Transitional Flat Plate(BC transition model)](/tutorials/Transitional_Flat_Plate/)
Simulation of external, transitional flow over a flat plate (transitional latminar-turbulent case).
* [Transitional Flat Plate(LM transition model)](/tutorials/Transitional_Flat_Plate/)
* [Transitional Flat Plate(LM transition model)](/tutorials/Transitional_Flat_Plate_T3A/)
Simulation of external, transitional flow over a flat plate(T3A & T3A-) (transitional latminar-turbulent case).
* [Turbulent ONERAM6](/tutorials/Turbulent_ONERAM6/)
Simulation of external, viscous flow around a 3D geometry (isolated wing) using a turbulence model.
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5 changes: 2 additions & 3 deletions _tutorials/multiphysics/steady_cht/Static_CHT.md
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Expand Up @@ -69,8 +69,7 @@ Uniform velocity boundary conditions are used for the farfield.

### Configuration File Options

Several of the key configuration file options for this simulation are highlighted here. First we show how we start a multiphysics simulation run incorporating CHT by choosing the following options in a main config file [cht_2d_3cylinders.cfg](https://github.com/su2code/Tutorials/tree/master/multiphysics/steady_cht/cht_2d_3cylinders.cfg) (see [https://su2code.github.io/docs/Multizone](https://su2code.github.io/docs/Multizone) how to setup a multiphysics simulation in general):

Several of the key configuration file options for this simulation are highlighted here. First we show how we start a multiphysics simulation run incorporating CHT by choosing the following options in a main config file [cht_2d_3cylinders.cfg](https://github.com/su2code/Tutorials/tree/master/multiphysics/steady_cht/cht_2d_3cylinders.cfg) (see [https://su2code.github.io/docs_v7/Multizone](https://su2code.github.io/docs_v7/Multizone) how to setup a multiphysics simulation in general):
```
MARKER_ZONE_INTERFACE= (cylinder_outer1, cylinder_inner1, cylinder_outer2, cylinder_inner2, cylinder_outer3, cylinder_inner3)
%
Expand Down Expand Up @@ -246,4 +245,4 @@ magnitude | heatflux value | FD derivative | rel. error (%)
1.0e-3 | -31.89682435269217 | 0.387001813 | 0.0906675
1.0e-4 | -31.89717268560501 | 0.386688997 | 0.0097636
1.0e-5 | -31.89720748792119 | 0.38665835 | 0.0018381
1.0e-6 | -31.89721096784924 | 0.38665548 | 0.001095
1.0e-6 | -31.89721096784924 | 0.38665548 | 0.001095