Program

Monday, September 26, 2016

Time Event  
08:00 - 09:00 Registration - Registration  
09:00 - 09:10 Opening (Amphitheater) - Welcome  
09:10 - 10:00 Invited keynote 1 (Amphitheater) - Shia-Hui Peng, Swedish Defence Research Agency, FOI, Sweden  
09:10 - 10:00 › Attached and Detached Eddy Simulation - Philippe Spalart, Boeing Commercial Airplanes, Seattle, USA
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10:00 - 10:30 Coffee break (Hall)  
10:30 - 12:10 Session 1 - A : Advances in HRLM (Amphitheater) - Shia-Hui Peng, Swedish Defence Research Agency, FOI, Sweden  
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 Session 1 - B : Numerics (Auditorium) - Stefan Wallin, KTH Stockholm  
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 Lunch (Hall)  
13:50 - 14:00 Tecplot (Amphitheater) - Yannick Hoarau, Strasbourg University  
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 Invited keynote 2 (Amphitheater) - Florian Menter, ANSYS Germany GmbH  
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 Session 2 - B : LES/SGS (Auditorium) - Sylvain Lardeau, CD-Adapco, UK  
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 Session 2 - A : Turbine (Amphitheater) - Florian Menter, ANSYS Germany GmbH  
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 Coffee break (Hall)  
16:35 - 17:25 Session 3 - A : Cylinder Flows (Amphitheater) - Mikhail K. Strelets, NTS, Saint-Petersburg  
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 Session 3 - B : Automotive (Auditorium) - Branislav Basara, AVL List GmbH  
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 Visit of the "Cave Historique des Hospices de Strasbourg" - http://www.vins-des-hospices-de-strasbourg.fr/  

Tuesday, September 27, 2016

Time Event  
09:00 - 09:50 Invited keynote 3 (Amphitheater) - Werner Haase, WHAC, Germany  
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 Session 4 - B : ELES (Auditorium) - Charles Mockett, CFD Software E+F GmbH, Germany  
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 Session 4 - A : High speed flow (Auditorium) - Werner Haase, WHAC, Germany  
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 Coffee break (Hall)  
11:35 - 12:50 Session 5 - A : LES/SGS (Amphitheater) - Dieter Schwamborn, Leiter C²A²S²E, DLR, Germany  
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 Session 5- B : FSI and Multiphysics (Auditorium) - Alistair Revell, Manchester University, UK  
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 Lunch (Hall)  
14:10 - 15:00 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 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 Coffee break (Hall)  
16:45 - 18:25 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]
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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
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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 Session 7 - B : Heat transfer (Auditorium) - Rémi Manceau, LMAP, France  
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]  
20:00 - 23:30 Conference dinner - http://www.maison-kammerzell.com/en  

Wednesday, September 28, 2016

Time Event  
09:00 - 09:50 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 Session 8 - A : High speed flow (Amphitheater) - Kozo Fujii, Tokyo University of Science, Japan  
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 Session 8 - B : Wind turbine (Auditorium) - Yannick Hoarau, Strasbourg University  
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 Coffee break (Hall)  
11:10 - 12:50 Session 9 : Aerodynamic applications (Amphitheater) - Philippe Spalart, Boeing Commercial Airplanes, USA  
11:10 - 11:35 › Multi-Disciplinary Analysis of Flow in Weapon Bays - Gaetan Loupy, University of Glasgow
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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 Closing remarks (Amphitheater)  
13:05 - 14:30 Lunch (Hall)  
  
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