Merge pull request #104 from su2code/master

update develop

Author: pcarruscag

_data/docs_v7.yml

@@ -40,6 +40,7 @@
   - Physical-Definition
   - Markers-and-BC
   - Convective-Schemes
+  - Slope-Limiters-and-Shock-Resolution
   - Custom-Output
   - Linear-Solvers-and-Preconditioners
   - Multizone

_data/tutorials.yml

@@ -12,6 +12,7 @@
   - Laminar_Cylinder
   - Turbulent_Flat_Plate
   - Transitional_Flat_Plate
+  - Transitional_Flat_Plate_T3A
   - Turbulent_ONERAM6
   - Unsteady_NACA0012
   - UQ_NACA0012

_data/vandv.yml

@@ -10,3 +10,4 @@
   - Bump_Channel
   - 30p30n
   - swbli
+  - LM_transition

_docs_v7/Physical-Definition.md

@@ -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)
 
 ---
 

_tutorials/compressible_flow/Transitional_Flat_Plate/Transitional_Flat_Plate_T3A_and_T3A-.md renamed to _tutorials/compressible_flow/Transitional_Flat_Plate_T3A/Transitional_Flat_Plate_T3A.md

@@ -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

_tutorials/index.md

@@ -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.

_tutorials/multiphysics/steady_cht/Static_CHT.md

@@ -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)
 %
@@ -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