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September, 24th, Wednesday |
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9:30-10:55 |
Joint Session 1 Chairman: Boris Chetverushkin, Keldysh Institute of Applied Mathematics RAS, Moscow, Russia |
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9:30-10:15 Invited lecture |
EFFICIENT HYBRID METHODS FOR COMPUTATIONAL AEROACOUSTICS IN COMPLEX ENVIRONMENTS Philip J. Morris and Yongle Du Penn State University, University Park, USA |
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10:15-10:35 |
Numerical simulation of the rotating instability in an axial compressor stator Christian Beselt2, Klaus Ehrenfried1, Ulf Michel1, Dieter Peitsch2, Ruben van Rennings1, Frank Thiele1 2Department of Aeronautics and Astronautics, Technische Universität Berlin, Germany |
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10:35-10:55 |
Time Resolved PIV measurements AND COMPUTATIONs OF A TIP LEAKAGE FLOW J.Boudet1, J.Caro1, N.Grosjean1, M.C.Jacob2, E.Jondeau1 2Laboratoire de Mécanique de Fluides et d’Acoustique, Polytech-Lyon/Université Claude Bernard Lyon 1/CNRS, Villeurbanne, France |
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11:15-12:35 |
Joint Session 2 Chairman: Mikhail Shur, St-Petersburg State Polytechnic University, St.-Petersburg, Russia |
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11:15-11:35 |
Progress IN NUMERICAL STUDIES ON ACOUSTICS OF TRANSITIONAL AIRFOILS Vladimir Golubev1, Michel Roger2, Reda Mankbadi3 3Embry-Riddle Aeronautical University, Daytona Beach, USA |
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11:35-11:55 |
DNS OF TRANSITION TO TURBULENCE IN COMPRESSIBLE MIXING LAYER ON HETEROGENEOUS COMPUTATIONAL CLUSTERS A.V.Kashkovsky1,2, A.N.Kudryavtsev1,2, A.A.Shershnev1,2 2Khristianovich Institute of Theoretical and Applied Mechanics SB RAS, Novosibirsk, Russia |
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11:55-12:15 |
MULTI-DISСIPLINARY NUMERICAL OPTIMISATION OF THE SLAT POSITION FOR A REALISTIC 2D HIGH LIFT AIRFOIL Thomas Le Garrec, Jean-Luc Godard, Eric Manoha, Daniel-Ciprian Mincu, Frederic Moens ONERA, The French Aerospace Lab, Châtillon, France |
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12:15-12:35 |
application OF GENETIC methods for surrogate modelling and airfoil shape optimization Ilya Evdokimov1, Valeryi Ivchin2 1“Russian Helicopters”, Moscow, Russia 2MIL Moscow Helicopter Plant, Russia |
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14:10-15:35 |
Joint Session 3 Chairman: Tatiana Kozubskaya, Keldysh Institute of Applied Mathematics RAS, Moscow, Russia |
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14:10-14:55 Invited lecture |
ROTORCRAFT AERODYNAMICS AND AEROACOUSTICS RESEARCH AT ONERA Blanche Demaret1, Yves Delrieux2, Arnaud Le Pape 3 , Philippe Beaumier 3 1Onera, Business Development Directorate, Palaiseau, France 2Onera, Computational Fluid Dynamics and Aeroacoustics, Chatillon, France 3Onera, Applied Aerodynamics Department, Meudon, France |
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14:55-15:15 |
Acoustic Comparison of Propellers C.S.Johnson, G.N.Barakos CFD Laboratory, School of Engineering, University of Liverpool, UK |
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15:15-15:35 |
NUMERICAL PREDICTION OF AERODYNAMIC AND AEROACOUSTIC CHARACTERISTICS OF AXISYMMETRICAL FLOW GENERATED BY SHROUDED TAIL ROTOR I.V.Abalakin1, V.A.Anikin2, P.A.Bakhvalov1, V.G.Bobkov1, T.K.Kozubskaya1 1Keldysh Institute of Applied Mathematics RAS, Moscow, Russia 2”Kamov”, Lubertsy, Russia |
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15:55-17:00 |
Joint Session 4 Chairman: Marc Jacob, Laboratoire de Mécanique de Fluides et d’Acoustique, Polytech-Lyon/Université Claude Bernard Lyon 1/CNRS, Villeurbanne, France |
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15:55-16:20 Commercial presentation |
ESI VIBRO-ACOUSTIC NUMERICAL SIMULATION SOLUTION Stanislav Vondraček MECAS ESI s.r.o., France |
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16:20-16:40 |
The exploration of numerical methods and noise modelling techniques applied to benchmark test cases with evaluation of their suitability for aeroacoustic design. Sergey Karabasov, Stanislav Proskurov, Vasily Semiletov School of Engineering and Materials Science, Queen Mary University of London, London, UK |
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16:40-17:00 |
Simulation of the Taylor-Green vortex decay using the DRP schemes Anatol Alexandrov1, Ludwig Dorodnicyn2 1Keldysh Institute of Applied Mathematics RAS, Moscow, Russia 2 Lomonosov Moscow State University, Moscow, Russia |
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September, 25th, Thursday |
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9:30-10:55 |
Joint Session 5 Chairman: Vladimir Titarev, Dorodnicyn Computing Centre RAS Moscow, Russia |
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9:30-10:15 Invited lecture |
Some LineariZed Perturbation equations for sound propagation Xin Zhang Airbus Noise Technology Centre, Faculty of Engineering and the Environment, Engineering Centre of Excellence, University of Southampton, UK |
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10:15-10:35 |
REAL ACCURACY OF MonOTONE AND NON-MONOTONE SHOCK CAPTURING SCHEMES FOR FLOWS WITH SHOCK WAVES O.A.Kovyrkina1, A.N.Kudryavtsev2,3, V.V.Ostapenko1 2Khristianovich Institute of Theoretical and Applied Mathematics SB RAS, Novosibirsk, Russia 3Novosibirsk State University, Novosibirsk, Russia |
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10:35-10:55 |
weno-EBR SCHEME FOR SOLVING AERODYNANICS AND AEROACOUSTICS PROBLEMS ON UNSTRUCTURED MESHES I.V.Abalakin, P.A.Bakhvalov, T.K.Kozubskaya Keldysh Institute of Applied Mathematics RAS, Moscow, Russia |
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11:15-12:40 |
Joint Session 6 Chairman: Ulf Michel, Institute of Fluid Dynamics and Engineering Acoustics, Technische Universität Berlin, Germany |
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11:15-12:00 Keynote presentation |
NONLINEAR WAVE PHENOMENA IN FLUIDS О.V. Rudenko Lomonosov Moscow State University, Moscow, Russia |
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COMPARATIVE ANALYSIS OF COUNTER-ROTATING PROPFANS NOISE ASSESSMENT METHODS IN THE CASE OF OPEN ROTOR WITH NARROW CYLINDRICAL SHIELD A.V.Gracheva, V.E.Makarov, K.S.Reent, V.A.Shorstov P.I.Baranov Central Institute of Aviation Motors, Moscow, Russia |
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12:20-12:40 |
theoretical and experimental investigations of the aircraft noise shielding by means of airframe structures S.L.Denisov, V.F.Kopiev, N.N.Ostrikov, M.Yu.Zaitsev Central Aerohydrodynamics Institute (TsAGI), Zhukovsky, Russia |
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14:10-15:30 |
Joint Session 7 Chairman: Vladimir Golubev, Embry-Riddle Aeronautical University, Daytona Beach, USA |
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14:10-14:30 |
Experimental investigation of noise radiated due to jet-wing interaction and the ways for itS suppresSion V.F.Kopiev, N.N.Ostrikov, M.Yu.Zaytsev Central Aerohydrodynamics Institute (TsAGI), Zhukovsky, Russia |
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14:30-14:50 |
On physical mechanisms responsible for excess noise due to jet-wing interaction O.P.Bychkov1,2, G.A.Faranosov1,3 3Perm National Research Polytechnic University, Perm, Russia |
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14:50-15:10 |
COMPUTATIONAL MODELLING OF JET-WING INSTALLATION NOISE S.A.Karabasov1, V.F.Kopiev1, V.A.Semiletov2, G.A.Faranosov1 1Central Aerohydrodynamics Institute (TsAGI), Zhukovsky, Russia 2School of Engineering and Materials Science, Queen Mary University of London, London, UK |
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15:10-15:30 |
Generation of Fluctuations by Transonic Flow over Shallow Cavity V.A.Lebiga, D.S.Mironov, A.Y.Pak, V.N.Zinoviev |
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15:50-16:55 |
Joint Session 8 Chairman: Sergey Karabasov, School of Engineering and Materials Science, Queen Mary University of London, London, UK |
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15:50-16:35 Invited lecture |
Prediction of Acoustics of Transonic Cavities using DES and SAS S.V.Babu, G.N.Barakos CFD Laboratory, University of Liverpool, Liverpool, UK |
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16:35-16:55 |
SIMULATIONs OF COMPRESSIBLE FLOWS ON UNSTRUCTURED MESHES A.Báez-Vidal1, J. B.Pedro1, O.Lehmkuhl2, F.X.Trias1, C.D.Pérez-Segarra1 1Heat and Mass Transfer Technological Center, Polytechnic University of Catalonia, Terrassa, Spain 2Termofluids S.L., Terrassa, Spain |
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September, 26th, Friday |
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9:30-10:35 |
Joint Session 9 Chairman: Alexey Mironov, P.I.Baranov Central Institute of Aviation Motors, Moscow, Russia |
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9:30-10:15 Invited lecture |
Numerical acoustics in Airbus: current status and future applications J.-Y.Suratteau, F.Wlassow Numerical Methods Group, Acoustic Department – EPA6, Toulouse, France |
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10:15-10:35 |
ON THE COMPUTATION OF AIRCRAFT ENGINE FAN NOISE GENERATION USING HIGH ORDER NUMERICAL METHODS ON GRAPHIC PROCESSING UNITS L.U.Gomzikov1, E.V.Koromyslov1,2,3, M.V.Usanin1, A.A.Siner1,2 1“Aviadvigatel”, Perm, Russia 3Institute of Continuous Media Mechanics UrB RAS, Perm, Russia |
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11:15-12:40 |
Joint Session 10 Chairman: Xin Zhang, Airbus Noise Technology Centre, Faculty of Engineering and the Environment, Engineering Centre of Excellence, University of Southampton, UK |
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11:15-12:00 Invited lecture |
Continuously Variable Fidelity Adaptive Large Eddy Simulation Oleg V. Vasilyev1, Alireza Nejadmalayeri1,2, Giuliano De Stefano3 1Department of Mechanical Engineering, University of Colorado, Boulder, USA 2FortiVenti Inc., Vancouver, Canada 3Dipartimento di Ingegneria Industriale e dell'Informazione,Seconda Università di Napoli, Aversa, Italy |
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12:00-12:20 |
JET NOISE COMPUTATION BASED ON ENHANCED DES FORMULATIONS acceleratIG RANS-to-LES transition IN FREE shear layers A.Garbaruk1, M.Shur1,2, P.R.Spalart3, M.Strelets1,2 3Boeing Commercial Airplanes, Seattle, USA |
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12:20-12:40 |
Jet noise modelling within a generalized acoustic analogy approach S.A.Karabasov1, V.A.Semiletov1, V.M.Goloviznin2 1Queen Mary University of London, London, UK 2Lomonosov Moscow State University, Moscow, Russia |
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14:10-15:10 |
Joint Session 11 Chairman: Mikhail Strelets, St-Petersburg State Polytechnic University, St.-Petersburg, Russia |
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14:10-14:30 |
LARGE SCALE STRUCTURES IN SUBSONIC tone EXCITED JET AND THEIR DIAGNOSTICS IN EXPERIMENT by viSualization AND IN NUMERICAL SIMULATIONS S.A.Chernyshev1, A.V.Garbaruk2, V.F.Kopiev1, M.L.Shur2, M.Kh.Strelets2 |
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14:30-14:50 |
Numerical Simulation of Supersonic Twin-jet noise with CAA method Junhui Gao, Xin Xu, Xiaodong Li |
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14:50-15:10 |
EMPIRICISM-FREE EVALUATION OF JET NOISE SOURCES BASED ON THE GENERALIZED ACOUSTIC ANALOGY AND SECOND-ORDER STATISTICS FROM LES DATA Vasily A. Semiletov, Sergey A. Karabasov Queen Mary University of London, London, UK |
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