Program
Monday, September 26, 2016
| Time |
Event |
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08:00 - 09:00
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Registration - Registration |
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09:00 - 09:10
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Opening (Amphitheater) - Welcome |
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09:10 - 10:00
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Invited keynote 1 (Amphitheater) - Shia-Hui Peng, Swedish Defence Research Agency, FOI, Sweden |
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| 09:10 - 10:00 |
› Attached and Detached Eddy Simulation - Philippe Spalart, Boeing Commercial Airplanes, Seattle, USA |
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10:00 - 10:30
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Coffee break (Hall) |
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10:30 - 12:10
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Session 1 - A : Advances in HRLM (Amphitheater) - Shia-Hui Peng, Swedish Defence Research Agency, FOI, Sweden |
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| 10:30 - 10:55 |
› Effect of upstream turbulence on single and dual-stream jets. Assessment of ZDES simulations - Fabien Gand, Onera - The French Aerospace Lab |
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| 10:55 - 11:20 |
› Implementation and Assessment of the Synthetic-Eddy Method in an Unstructured Compressible Flow Solver - Axel Probst, German Aerospace Center |
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| 11:20 - 11:45 |
› Hybrid RANS/LES Simulation Strategy for High-Lift Applications with Disturbed Inflow - Silvia Reuss, German Aerospace Center |
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| 11:45 - 12:10 |
› Grey-area mitigation using commutation terms at the interfaces in hybrid RANS-LES modeling - Sebastian Arvidson, Chalmers University of Technology/Saab Aeronautics |
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10:30 - 12:10
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Session 1 - B : Numerics (Auditorium) - Stefan Wallin, KTH Stockholm |
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| 10:30 - 10:55 |
› Effects of convection schemes on hybrid RANS-LES calculations - Branislav Basara, AVL List GmbH |
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| 11:20 - 11:45 |
› Application of a stochastic backscatter model for grey-area mitigation in detached eddy simulations - Johan Kok, Netherlands Aerospace Centre [Amsterdam] |
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| 11:45 - 12:10 |
› 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 |
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12:10 - 13:50
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Lunch (Hall) |
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13:50 - 14:00
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Tecplot (Amphitheater) - Yannick Hoarau, Strasbourg University |
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| 13:50 - 14:00 |
› Strategies to post-process big datasets. - Antoine Ligier, Genias Graphics GmbH & Co. KG |
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14:00 - 14:50
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Invited keynote 2 (Amphitheater) - Florian Menter, ANSYS Germany GmbH |
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| 14:00 - 14:50 |
› Progress in Hybrid Temporal LES - Rémi Manceau, Laboratoire de Mathématiques et de leurs Applications [Pau] |
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14:50 - 16:05
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Session 2 - B : LES/SGS (Auditorium) - Sylvain Lardeau, CD-Adapco, UK |
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| 14:50 - 15:15 |
› Reynolds-constrained Subgrid-scale Modelling for Large-eddy Simulation of Turbulent Wall Flows - Zuoli Xiao, Peking University |
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| 15:15 - 15:40 |
› Scale-Resolving Simulations Based on a Lattice-Boltzmann Method - Benjamin Duda, Exa GmbH |
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14:50 - 16:05
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Session 2 - A : Turbine (Amphitheater) - Florian Menter, ANSYS Germany GmbH |
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| 14:50 - 15:15 |
› Assessment of Scale-Resolving Simulations for Turbomachinery Applications - Martin Franke, German Aerospace Center |
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| 15:15 - 15:40 |
› Comparison of Hybrid RANS/LES Methods for Supersonic Combustion in a Model Scramjet Combustor - Junsu Shin, Korea Aerospace University |
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| 15:40 - 16:05 |
› Computational Investigation of a Swirled Premixed Burner Using Hybrid RANS-LES method - zakaria mansouri, Institut de Combustion Aérothermique Réactivité et Environnement |
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16:05 - 16:35
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Coffee break (Hall) |
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16:35 - 17:25
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Session 3 - A : Cylinder Flows (Amphitheater) - Mikhail K. Strelets, NTS, Saint-Petersburg |
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| 16:35 - 17:00 |
› Numerical simulation of flow past an oscillating rod-airfoil configuration - WenQing Zhu, Tsinghua University [Beijing] |
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| 17:00 - 17:25 |
› Modelled and Resolved Turbulent Stresses around a circular cylinder using DES and DDES - Naveed Durrani, Centres of Excellence in Science and Applied Technologies |
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16:35 - 17:50
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Session 3 - B : Automotive (Auditorium) - Branislav Basara, AVL List GmbH |
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| 16:35 - 17:00 |
› Assessment of turbulence models for flow around three-dimensional geometries - Emmanuel Guilmineau, LHEEA, CNRS UMR 6598, Ecole Centrale de Nantes |
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| 17:00 - 17:25 |
› Comparisons of 3 hybrid turbulence models for the flow around a 25° Ahmed body - François Delassaux, CNAM Paris |
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18:30 - 20:00
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Visit of the "Cave Historique des Hospices de Strasbourg" - http://www.vins-des-hospices-de-strasbourg.fr/ |
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Tuesday, September 27, 2016
| Time |
Event |
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09:00 - 09:50
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Invited keynote 3 (Amphitheater) - Werner Haase, WHAC, Germany |
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| 09:00 - 09:50 |
› Stress-Blended Eddy Simulation (SBES) - A new Paradigm in hybrid RANS-LES Modeling - Florian Menter, ANSYS Germany GmbH |
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09:50 - 11:05
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Session 4 - B : ELES (Auditorium) - Charles Mockett, CFD Software E+F GmbH, Germany |
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| 10:15 - 10:40 |
› Application of Embedded Simulation Methods to Internal Pipe Flows - Joshua Holgate, School of Mechanical Aerospace and Civil Engineering |
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09:50 - 11:05
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Session 4 - A : High speed flow (Auditorium) - Werner Haase, WHAC, Germany |
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| 09:50 - 10:15 |
› Numerical simulation and hybrid modelling of a 3-D laminar wing in transonic regime - M. Braza, Institut de mécanique des fluides de Toulouse |
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| 10:15 - 10:40 |
› Hybrid RANS-LES study of transonic flow in the wake of a generic space launch vehicle - Tim Horchler, German Aerospace Center |
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11:05 - 11:35
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Coffee break (Hall) |
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11:35 - 12:50
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Session 5 - A : LES/SGS (Amphitheater) - Dieter Schwamborn, Leiter C²A²S²E, DLR, Germany |
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| 11:35 - 12:00 |
› Can anisotropy-resolving SGS models relax the resolution requirements in hybrid RANS-LES? - Stefan Wallin, Linne FLOW Centre, KTH Mechanics, Stockholm |
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| 12:00 - 12:25 |
› A Multi-Scale Gas-Kinetic Scheme for Turbulence Simulation - Shuang Tan, Tsinghua University |
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11:35 - 12:50
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Session 5- B : FSI and Multiphysics (Auditorium) - Alistair Revell, Manchester University, UK |
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| 11:35 - 12:00 |
› Numerical study of 3D turbulent cavitating flows - Eric Goncalves, Institut P' CNRS - Université de Poitiers - ENSMA UPR 3346 SP2MI |
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| 12:00 - 12:25 |
› Predictions of turbulence and acoustics from an ultra- bypass serrated nozzle using hybrid RANS-LES - Zhong-Nan Wang, Engineering Department |
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| 12:25 - 12:50 |
› Cross flow induced vibration in a single tube of square array using Large Eddy Simulation - Vilas Shinde, Institut des Sciences de la Mécanique et Applications Industrielles Institut des Sciences de la Mécanique et Applications Industrielles |
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12:50 - 14:10
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Lunch (Hall) |
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14:10 - 15:00
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Invited keynote 4 (Amphitheater) - Suad Jakirlic, Technische Universität Darmstadt, Germany |
|
| 14:10 - 15:00 |
› Consistent strain/stress lag eddy-viscosity model for hybrid RANS/LES - Sylvain Lardeau, CD-adapco |
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15:00 - 16:15
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Session 6 : Airfoil/BL (Amphitheater) - Suad Jakirlic, Technische Universität Darmstadt, Germany |
|
| 15:00 - 15:25 |
› Detached Eddy Simulation of an SD7003 Airfoil - Eike Tangermann, Numerical Methods in Aerospace Engineering, Universität der Bundeswehr München |
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| 15:25 - 15:50 |
› Vortex breakdown flows around a double-delta wing during pitching motion based on DDES - zhixiang xiao, School of Aerospace Engineering,Tsinghua University |
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| 15:50 - 16:15 |
› On the convection velocity of wall-bounded turbulence resolved by ZDES mode III at Reθ = 13 000 - Nicolas Renard, Onera - The French Aerospace Lab |
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16:15 - 16:45
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Coffee break (Hall) |
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16:45 - 18:25
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Session 7 - A : Advances in HRLM (Amphitheater) - Song Fu, Tsinghua University, China |
|
| 16:45 - 17:10 |
› On the von Karman length scale as a triggering parameter in eddy-resolving simulations of turbulent flows - Suad Jakirlic, Darmstadt University of Technology [Darmstadt] |
|
| 17:10 - 17:35 |
› Recent results with grey-area improved DDES for a wide range of flows - Charles Mockett - CFD Software Entwicklungs- und Forschungsgesellschaft mbH |
|
| 17:35 - 18:00 |
› Hybrid simulation of high-Reynolds number flows relying on variational multiscale model - Emmanuelle ITAM, IMAG, Université de Montpellier |
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| 18:00 - 18:25 |
› A control strategy of the actual resolution in hybrid RANS/LES methods - Christophe Friess, Laboratoire de Mécanique, Modélisation et Procédés Propres |
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16:45 - 18:25
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Session 7 - B : Heat transfer (Auditorium) - Rémi Manceau, LMAP, France |
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| 17:10 - 17:35 |
› Experimental and numerical investigation of a heated impinging jet for a small nozzle-to-plate distance and high Reynolds number - Fabien Gand, Onera - The French Aerospace Lab |
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| 17:35 - 18:00 |
› An algebraic hybrid RANS-LES model with application to turbulent heat transfer - Ilyas Yilmaz, Mechanical Eng. Dept., Istanbul Aydin University |
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| 18:00 - 18:25 |
› Comparison of Hybrid RANS-LES Simulations of Turbulent Flow and Heat Transfer in a Ribbed Duct - Sung in Kim, Queen's University Belfast [Belfast] |
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20:00 - 23:30
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Conference dinner - http://www.maison-kammerzell.com/en |
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Wednesday, September 28, 2016
| Time |
Event |
|
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09:00 - 09:50
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Invited keynote 5 (Amphitheater) - Kozo Fujii, Tokyo University of Science, Japan |
|
| 09:00 - 09:50 |
› Detached-Eddy Simulations for active flow control - Song Fu, Tsinghua University |
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09:50 - 10:40
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Session 8 - A : High speed flow (Amphitheater) - Kozo Fujii, Tokyo University of Science, Japan |
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| 09:50 - 10:15 |
› Hybrid RANS/LES simulation of a supersonic coaxial He/Air jet experiment with variable turbulent Prandtl and Schmidt numbers - Lorris Charrier, Airbus Defence & Space |
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| 10:15 - 10:40 |
› Hybrid RANS/LES simulation of a space launcher using an high order finite volume scheme and grid intersections technique - Grégoire Pont, Airbus Defence & Space |
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09:50 - 10:40
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Session 8 - B : Wind turbine (Auditorium) - Yannick Hoarau, Strasbourg University |
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| 09:50 - 10:15 |
› Detached-eddy simulation of a horizontal axis wind turbine - Amin Rasam, Royal Institute of Technology |
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| 10:15 - 10:40 |
› Hybrid RANS/LES capabilities of the Flow Solver FLOWer - Application to Flow around Wind Turbines - Pascal Weihing, Institute of Aerodynamics and Gas Dynamics, University of Stuttgart |
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10:40 - 11:10
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Coffee break (Hall) |
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11:10 - 12:50
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Session 9 : Aerodynamic applications (Amphitheater) - Philippe Spalart, Boeing Commercial Airplanes, USA |
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| 11:10 - 11:35 |
› Multi-Disciplinary Analysis of Flow in Weapon Bays - Gaetan Loupy, University of Glasgow |
|
| 11:35 - 12:00 |
› Parametric Study of Cavity Leading-edge Rod Spoilers by Advanced Hybrid RANS-LES Methods - Kunyu Luo, Tsinghua University [Beijing] |
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| 12:00 - 12:25 |
› Hybrid RANS-LES Turbulence Modelling in Aeroelastic Problems, Test Case 3 from the Second AIAA Aeroelastic Prediction Workshop - Marcello Righi, Zurich University of Applied Sciences |
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| 12:25 - 12:50 |
› Improvement of CFD-Wind Tunnel Correlation near Buffet Onset by Using Scale Resolving Simulations - Marius-Gabriel Cojocaru, National Institute of Aerospace Research “Elie Carafoli” (INCAS) , Bucharest, Romania |
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12:50 - 13:05
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Closing remarks (Amphitheater) |
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13:05 - 14:30
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Lunch (Hall) |
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