|
| 1 | +--- |
| 2 | +title: Langtry and Menter transition model |
| 3 | +permalink: /vandv/LM_transition/ |
| 4 | +--- |
| 5 | + |
| 6 | +| Solver | Version | Author | |
| 7 | +| --- | --- | --- | |
| 8 | +| `RANS` | 7.4.0 | S. Kang | |
| 9 | + |
| 10 | +The details of the Langtry and Menter(LM) transition model validation cases are taken from the [AIAA Transition modeling workshop-I](https://transitionmodeling.larc.nasa.gov). |
| 11 | +To validate the LM model, the simulation results of SU2 are compared with the results of Fluent19.0 with a similar numerical setting. |
| 12 | + |
| 13 | +## Problem Setup |
| 14 | + |
| 15 | + |
| 16 | +Flow conditions are the reference from : https://doi.org/10.2514/6.2022-3679 and [AIAA Transition modeling workshop-I](https://transitionmodeling.larc.nasa.gov). |
| 17 | + |
| 18 | +| Case | T3A | T3B | T3Am | NLF0416| |
| 19 | +| --- | --- | --- | --- | --- | |
| 20 | +|Inlet Velocity (m/s)| 69.44 | 69.44 | 19.8 | 34.72 | |
| 21 | +| --- | --- | --- | --- | --- | |
| 22 | +|Density (kg/m^3) | 0.053 | 0.053 | 1.2 | 2.13 | |
| 23 | +| --- | --- | --- | --- | --- | |
| 24 | +|Viscosity (kg/ms) | 1.85E-5 | 1.85E-5 | 1.79E-5 | Sutherland's Law | |
| 25 | +| --- | --- | --- | --- | --- | |
| 26 | +|Freestream Temperature (K) | 300 | 300 | 300 | 300 | |
| 27 | +| --- | --- | --- | --- | --- | |
| 28 | +|Unit Reynolds number (1/m) | 2.0E5 | 2.0E5 | 1.328E6 | 4.0E6 | |
| 29 | +| --- | --- | --- | --- | --- | |
| 30 | +|Mach Number | 0.2 | 0.2 | 0.058 | 0.1 | |
| 31 | +| --- | --- | --- | --- | --- | |
| 32 | +|AoA | 0.0 | 0.0 | 0.0 | 0.0 | |
| 33 | +| --- | --- | --- | --- | --- | |
| 34 | +|Viscosity Ratio| 11.9 | 99.0 | 9.0 | 1.0 | |
| 35 | +| --- | --- | --- | --- | --- | |
| 36 | +|Freestream Turbulence Intensity (%) | 5.855 | 7.216 | 1.0 | 0.15 | |
| 37 | + |
| 38 | + |
| 39 | +## Mesh Description |
| 40 | + |
| 41 | +The grids of T3A, T3B, and NLF cases are provided by [TMW](https://transitionmodeling.larc.nasa.gov/workshop_i/)(Transition Model Workshop). And, The grid of T3Am was made with reference to https://doi.org/10.2514/6.2022-3679. |
| 42 | +If you would like to run the above cases for yourself, you can use only the fine level grid files available in the [SU2 V&V repository]https://github.com/su2code/VandV/tree/master/rans/flatplate). |
| 43 | + |
| 44 | + |
| 45 | +## Numerical Scheme |
| 46 | + |
| 47 | +| | Fluent | SU2 | |
| 48 | +| Flux | Roe-FDS | L2ROE | |
| 49 | +| --- | --- | --- | |
| 50 | +| Gradient | Least Squares Cell Based | WEIGHTED_LEAST_SQUARES | |
| 51 | +| --- | --- | --- | |
| 52 | +| Spatial Discretization Flow | Third-order MUSCL | MUSCL_FLOW | |
| 53 | +| --- | --- | --- | |
| 54 | +| Spatial Discretization Turbulence | Third-order MUSCL | MUSCL_YES | |
| 55 | +| --- | --- | --- | |
| 56 | + |
| 57 | +## Results |
| 58 | + |
| 59 | +Present results of all grid resolutions and then plot the results of the fine-level grid separately. If you want to see other results of the gird level, you can see them at "vandv_files/LMmodel". |
| 60 | + |
| 61 | +### T3A |
| 62 | +The experiment data from [here]http://web.tecnico.ulisboa.pt/ist12278/Workshop_AVT_313_2D_cases/html_files/Flat_Plate.htm |
| 63 | +C : Coarse |
| 64 | +M : Medium |
| 65 | +F : Fine |
| 66 | +X : Extra fine |
| 67 | + |
| 68 | +<p align="center"> |
| 69 | +<img src="/vandv_files/LM_model/T3A/All_Cf.png" alt="All result comparsion of Cf distribution on T3A" /> |
| 70 | +<img src="/vandv_files/LM_model/T3A/Fine_Cf.png" alt="Fine level result comparsion of Cf distribution on T3A" /> |
| 71 | + |
| 72 | +### T3B |
| 73 | + |
| 74 | + |
| 75 | +### T3Am |
| 76 | + |
| 77 | + |
| 78 | +### NLF0416 |
| 79 | + |
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