AIAA Aviation 2019 Forum 2019
DOI: 10.2514/6.2019-3059
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Unstructured anisotropic mesh adaptation for 3D RANS turbomachinery applications

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Cited by 5 publications
(4 citation statements)
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“…This data is presented in Figure 5. 27 The initial mesh CHAPTER 5 M 0 being rather coarse, it does not allow for the solving of the physics in the near wall region correctly. This explains the low shear values.…”
Section: Discussion Of Aerothermal Resultsmentioning
confidence: 99%
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“…This data is presented in Figure 5. 27 The initial mesh CHAPTER 5 M 0 being rather coarse, it does not allow for the solving of the physics in the near wall region correctly. This explains the low shear values.…”
Section: Discussion Of Aerothermal Resultsmentioning
confidence: 99%
“…Mesh adaptation appears as one of the most promising techniques for optimized grid generation [48]. While extensive work has been done for Reynolds-Averaged Navier-Stokes simulations (RANS) [33,25,13,3,27], the unsteady nature of the LES equations challenges the generation of the optimal grid. In Chapter 3, two main feature-based approaches have been developed, namely dynamic or static mesh refinement (DMR vs SMR).…”
Section: A Mesh Adaptation Strategy Ensuring Independent Mean Kinetic...mentioning
confidence: 99%
“…Mesh adaptation appears as one of the most promising techniques for optimized mesh generation [18]. While extensive work has been done for Reynolds-Averaged Navier-Stokes simulations (RANS) [19][20][21][22][23], the unsteady nature of the LES equations challenges the generation of the optimal mesh. Two main feature-based approaches have been developed, namely Dynamic or Static Mesh Refinement (hereinafter called DMR and SMR).…”
Section: Introductionmentioning
confidence: 99%
“…With adaptive refinement, the mesh is changed dynamically during a simulation, to adapt it to the requirements of the evolving flow field. AGR today is used frequently and reliably in RANS simulations for different applications, such as aerodynamics [2,3,19], free surface capturing [40,43], reacting flows [10] and in turbo-machinery configurations [9,38].…”
Section: Introductionmentioning
confidence: 99%