Tanarro Á, Mallor F, Offermans N, Peplinski A, Vinuesa R, Schlatter P (2019)
Publication Type: Conference contribution
Publication year: 2019
Publisher: International Symposium on Turbulence and Shear Flow Phenomena, TSFP
Conference Proceedings Title: 11th International Symposium on Turbulence and Shear Flow Phenomena, TSFP 2019
Event location: Southampton, GBR
The implementation of adaptive mesh refinement (AMR) in Nek5000 is used for the first time on the simulation of the flow over wings. This is done by simulating the flow over a NACA4412 profile with 5° angle of attack at chord-based Reynolds number 200,000. The mesh is progressively refined by means of AMR which allows for high resolution near the wall whereas significantly larger elements are used in the far-field. The resultant mesh shows higher resolution than previous conformal meshes, and it allows for larger computational domains, which avoid the use of RANS to determine the boundary condition, all of this with, approximately, 3 times lower total number of grid points. The results of the turbulence statistics show a good agreement with the ones obtained with the conformal mesh. Finally, using AMR on wings leads to simulations at higher Reynolds numbers (i.e. Re
APA:
Tanarro, Á., Mallor, F., Offermans, N., Peplinski, A., Vinuesa, R., & Schlatter, P. (2019). Using adaptive mesh refinement to simulate turbulent wings at high Reynolds numbers. In 11th International Symposium on Turbulence and Shear Flow Phenomena, TSFP 2019. Southampton, GBR: International Symposium on Turbulence and Shear Flow Phenomena, TSFP.
MLA:
Tanarro, Álvaro, et al. "Using adaptive mesh refinement to simulate turbulent wings at high Reynolds numbers." Proceedings of the 11th International Symposium on Turbulence and Shear Flow Phenomena, TSFP 2019, Southampton, GBR International Symposium on Turbulence and Shear Flow Phenomena, TSFP, 2019.
BibTeX: Download