Update Index

Update Index

Author: sun5k

_tutorials/index.md

@@ -36,9 +36,9 @@ Simulation of external, inviscid flow around a 3D geometry (isolated wing).
 Simulation of external, laminar flow over a flat plate (classical Navier-Stokes validation).
 * [Laminar Cylinder](/tutorials/Laminar_Cylinder/)    
 Simulation of external, laminar flow around a 2D cylinder.
-* [Turbulent Flat Plate](/tutorials/Turbulent_Flat_Plate/)    
+* [Turbulent Flat Plate for BC transition model](/tutorials/Turbulent_Flat_Plate/)    
 Simulation of external, turbulent flow over a flat plate (classical RANS validation).
-* [Transitional Flat Plate](/tutorials/Transitional_Flat_Plate/)    
+* [Transitional Flat Plate for Langtry and Menter transition model](/compressible_flow/Transitional_Flat_Plate/)    
 Simulation of external, transitional flow over a flat plate (transitional latminar-turbulent case).
 * [Turbulent ONERAM6](/tutorials/Turbulent_ONERAM6/)     
 Simulation of external, viscous flow around a 3D geometry (isolated wing) using a turbulence model.

_vandv/index.md

@@ -19,13 +19,15 @@ We will continue to add cases over time to demonstrate V&V of additional physica
 
 #### Compressible Flow
 
-* [Method of Manufactured Solutions for Compressible Navier-Stokes](/vandv/MMS_FVM_Navier_Stokes/)
+* [Method of Manufactured Solutions for Compressible Navier-Stokes](/_vandv/MMS_FVM_Navier_Stokes/)
 Formal order of accuracy of the finite volume solver in SU2 for the laminar Navier-Stokes equations is assessed.
-* [2D Zero Pressure Gradient Flat Plate RANS Verification Case](/vandv/Flat_Plate/)
+* [2D Zero Pressure Gradient Flat Plate RANS Verification Case](/_vandv/Flat_Plate/)
 Code-to-code comparisons of drag and skin friction on a turbulent flat plate is presented using data from the NASA Turbulence Modeling Resource.
-* [2D Bump-in-Channel RANS Verification Case](/vandv/Bump_Channel/)
+* [2D Bump-in-Channel RANS Verification Case](/_vandv/Bump_Channel/)
 Code-to-code comparisons for a bump in a channel, which results in pressure gradients, is presented using data from the NASA Turbulence Modeling Resource.
-* [Three-Element High-Lift Subsonic Airfoil](/vandv/30p30n/)
+* [Three-Element High-Lift Subsonic Airfoil](/_vandv/30p30n/)
 Results for the 30p30n airfoil, mesh independence study at low angle-of-attack, and determination of maximum lift, both comparing different numerical schemes.
-* [Shock-Wave Boundary-Layer Interaction](/vandv/swbli/)
+* [Shock-Wave Boundary-Layer Interaction](/_vandv/swbli/)
 Comparison of grid-converged results with experimental data. SA and SST turbulence models.
+* [2D Transition Flat Plate (T3A & T3A-) for Langtry and Menter transition model](/_vandv/LM_transition/)
+Comparison of grid-converged results with results of another solver and experimental data.