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Merged
merged 10 commits into from
May 4, 2025
Merged

update develop #174

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286bbd7
website page for the dsma661 v&v case
Bot-Enigma-0 Mar 22, 2025
eb68aea
Update index.md
Bot-Enigma-0 Mar 22, 2025
fdaede6
Merge pull request #170 from Bot-Enigma-0/master
pcarruscag Mar 24, 2025
7343563
Update dsma661.md to add dropdown menu
Bot-Enigma-0 Mar 24, 2025
79cebcf
Update index.md to add case to dropdown menu
Bot-Enigma-0 Mar 24, 2025
939b40f
Update vandv.yml to add case to dropdown menu
Bot-Enigma-0 Mar 24, 2025
e82a04f
Merge pull request #171 from Bot-Enigma-0/master
pcarruscag Mar 24, 2025
c0e2631
updated sst results
Bot-Enigma-0 Mar 25, 2025
06bb620
Merge pull request #173 from su2code/develop
pcarruscag May 4, 2025
c0d0ea9
Merge pull request #172 from Bot-Enigma-0/master
pcarruscag May 4, 2025
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5 changes: 3 additions & 2 deletions _data/vandv.yml
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Expand Up @@ -11,7 +11,8 @@
- 30p30n
- swbli
- LM_transition

- dsma661

- title: Incompressible Flow
vandv:
- SANDIA_jet
- SANDIA_jet
4 changes: 2 additions & 2 deletions _vandv/dsma661.md
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@@ -1,6 +1,6 @@
---
title: 2D DSMA661 Airfoil Near-Wake RANS Verification Case
permalink: /vandv/DSMA661/
permalink: /vandv/dsma661/
---

| Solver | Version |
Expand Down Expand Up @@ -238,4 +238,4 @@ Additional codes have been compared against the FUN3D and CFL3D results, and are
<p align="center">
<img src="/vandv_files/dsma661/images/sst/comp_skinfric_coeff.png" alt="Airfoil Surface Skin Friction Coefficient on Finest Grid">
</p>
**Figure (46)**: Airfoil Surface Skin Friction Coefficient on Finest Grid
**Figure (46)**: Airfoil Surface Skin Friction Coefficient on Finest Grid
2 changes: 1 addition & 1 deletion _vandv/index.md
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Expand Up @@ -31,7 +31,7 @@ Results for the 30p30n airfoil, mesh independence study at low angle-of-attack,
Comparison of grid-converged results with experimental data. SA and SST turbulence models.
* [2D 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.
* [2D DSMA661 Airfoil Near-Wake RANS Verification Case](/vandv/DSMA661/)
* [2D DSMA661 Airfoil Near-Wake RANS Verification Case](/vandv/dsma661/)
Code-to-Code comparisons of grid-converged results of lift, drag and wake profile plots is presented using data from the NASA Turbulence Modeling Resource.


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