6th Symposium on Hybrid RANS-LES Methods

Registration

Opening

Amphitheater

Welcome

Invited keynote 1

Amphitheater

Shia-Hui Peng, Swedish Defence Research Agency, FOI, Sweden

› Attached and Detached Eddy Simulation - Philippe Spalart, Boeing Commercial Airplanes, Seattle, USA 09:10-10:00 (50min)

Coffee break

Hall

Session 1 - A : Advances in HRLM

Amphitheater

Shia-Hui Peng, Swedish Defence Research Agency, FOI, Sweden

› Effect of upstream turbulence on single and dual-stream jets. Assessment of ZDES simulations - Fabien Gand, Onera - The French Aerospace Lab 10:30-10:55 (25min)

› Implementation and Assessment of the Synthetic-Eddy Method in an Unstructured Compressible Flow Solver - Axel Probst, German Aerospace Center 10:55-11:20 (25min)

› Hybrid RANS/LES Simulation Strategy for High-Lift Applications with Disturbed Inflow - Silvia Reuss, German Aerospace Center 11:20-11:45 (25min)

› Grey-area mitigation using commutation terms at the interfaces in hybrid RANS-LES modeling - Sebastian Arvidson, Chalmers University of Technology/Saab Aeronautics 11:45-12:10 (25min)

Session 1 - B : Numerics

Auditorium

Stefan Wallin, KTH Stockholm

› Effects of convection schemes on hybrid RANS-LES calculations - Branislav Basara, AVL List GmbH 10:30-10:55 (25min)

› Application of a stochastic backscatter model for grey-area mitigation in detached eddy simulations - Johan Kok, Netherlands Aerospace Centre [Amsterdam] 11:20-11:45 (25min)

› On scale-resolving simulation of turbulent flows using higher-accuracy quasi-1D schemes on unstructured meshes - Alexey Duben, Keldysh Institute of Applied Mathematics of RAS 11:45-12:10 (25min)

Lunch

Hall

Tecplot

Amphitheater

Yannick Hoarau, Strasbourg University

› Strategies to post-process big datasets. - Antoine Ligier, Genias Graphics GmbH & Co. KG 13:50-14:00 (10min)

Invited keynote 2

Amphitheater

Florian Menter, ANSYS Germany GmbH

› Progress in Hybrid Temporal LES - Rémi Manceau, Laboratoire de Mathématiques et de leurs Applications [Pau] 14:00-14:50 (50min)

Session 2 - A : Turbine

Amphitheater

Florian Menter, ANSYS Germany GmbH

› Assessment of Scale-Resolving Simulations for Turbomachinery Applications - Martin Franke, German Aerospace Center 14:50-15:15 (25min)

› Comparison of Hybrid RANS/LES Methods for Supersonic Combustion in a Model Scramjet Combustor - Junsu Shin, Korea Aerospace University 15:15-15:40 (25min)

› Computational Investigation of a Swirled Premixed Burner Using Hybrid RANS-LES method - zakaria mansouri, Institut de Combustion Aérothermique Réactivité et Environnement 15:40-16:05 (25min)

Session 2 - B : LES/SGS

Auditorium

Sylvain Lardeau, CD-Adapco, UK

› Reynolds-constrained Subgrid-scale Modelling for Large-eddy Simulation of Turbulent Wall Flows - Zuoli Xiao, Peking University 14:50-15:15 (25min)

› Scale-Resolving Simulations Based on a Lattice-Boltzmann Method - Benjamin Duda, Exa GmbH 15:15-15:40 (25min)

Coffee break

Hall

Session 3 - A : Cylinder Flows

Amphitheater

Mikhail K. Strelets, NTS, Saint-Petersburg

› Numerical simulation of flow past an oscillating rod-airfoil configuration - WenQing Zhu, Tsinghua University [Beijing] 16:35-17:00 (25min)

› Modelled and Resolved Turbulent Stresses around a circular cylinder using DES and DDES - Naveed Durrani, Centres of Excellence in Science and Applied Technologies 17:00-17:25 (25min)

Session 3 - B : Automotive

Auditorium

Branislav Basara, AVL List GmbH

› Assessment of turbulence models for flow around three-dimensional geometries - Emmanuel Guilmineau, LHEEA, CNRS UMR 6598, Ecole Centrale de Nantes 16:35-17:00 (25min)

› Comparisons of 3 hybrid turbulence models for the flow around a 25° Ahmed body - François Delassaux, CNAM Paris 17:00-17:25 (25min)

Visit of the "Cave Historique des Hospices de Strasbourg"

Program