Multi-level Approach
| Autor: | P. Yser, Fabio Naddei, M. de la Llave Plata, Eric Lamballais, F. Chalot |
|---|---|
| Přispěvatelé: | DMPE, ONERA, Université Paris Saclay [Châtillon], ONERA-Université Paris-Saclay, Dassault Aviation, Institut Pprime (PPRIME), Université de Poitiers-ENSMA-Centre National de la Recherche Scientifique (CNRS), European Project: 635962,H2020,H2020-MG-2014_TwoStages,TILDA(2015) |
| Jazyk: | angličtina |
| Rok vydání: | 2021 |
| Předmět: |
Variational multiscale LES
Computer science Reference data (financial markets) Direct numerical simulation Context (language use) 01 natural sciences 010305 fluids & plasmas symbols.namesake [SPI]Engineering Sciences [physics] Finite element Discontinuous Galerkin method 0502 economics and business 0103 physical sciences [INFO]Computer Science [cs] Aerospace engineering Large Eddy Simulation LES [PHYS]Physics [physics] business.industry 05 social sciences Reynolds number Variational multiscale approach VMS Vortex Flow (mathematics) symbols business Scale model 050203 business & management |
| Zdroj: | TILDA: Towards Industrial LES/DNS in Aeronautics TILDA: Towards Industrial LES/DNS in Aeronautics, 148, Springer International Publishing, pp.63-102, 2021, Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 978-3-030-62047-9. ⟨10.1007/978-3-030-62048-6_3⟩ Notes on Numerical Fluid Mechanics and Multidisciplinary Design ISBN: 9783030620479 |
| DOI: | 10.1007/978-3-030-62048-6_3⟩ |
| Popis: | International audience; In the framework of the TILDA project, Dassault Aviation and ONERA have worked on the development of variational multiscale (VMS) approaches to LES in the context of high-order, respectively continuous and discontinuous Galerkin, Finite-Element methods. Dassault Aviation presents the implementation of VMS in its higher-order industrial stabilized continuous finite-element code AeTher, whereas ONERA investigates the performance of the VMS approach based on a high-order DG method. Both authors assess the numerical developments with the Taylor-Green vortex test case at different Reynolds numbers ranging from 1500 to 20,000. VMS results are compared with reference data provided by direct numerical simulation and with simulations obtained using various subgrid scale models and numerical fluxes. LES simulations of the sub-critical flow past a circular cylinder at Reynolds 3900 and 20,000 have also been considered by ONERA. |
| Databáze: | OpenAIRE |
| Externí odkaz: |
|