Program

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Workshop Schedule

Dates:                      September 17-22, 2012
Date of arrival:           September 18, 2012 (Tuesday)
Date of departure:     September 23, 2012 (Sunday)

September 18, Tuesday         Arrival
September 19, Wednesday    First working day, Svetlogorsk; Welcome reception, Kaliningrad
September 20, Thursday        Second working day, Svetlogorsk
September 21, Friday             Third working day, Svetlogorsk; Banquet, Svetlogorsk
September 22, Saturday        Outdoor and round-table discussions within bus excursion trip in Kaliningrad region
September 23, Sunday          Departure


PRELIMINARY PROGRAM:  PDF


 

List of talks accepted (in alphabetical order):

  • Edge-Based Reconstruction Scheme and its WENO Implementation for Solving Aerodynamics and Aeroacoustics Problems on Unstructured Tetrahedral Meshes
    Ilya Abalakin1, Pavel Bakhvalovl2, Tatiana Kozubskaya1
    1Keldysh Institute of Applied Mathematics RAS, Moscow, Russia
    2Moscow Institute of Physics and Technology, Dolgoprudny, Moscow region, Russia
  • Airframe Noise Simulation Using Supercomputer Technologies
    Ilya Abalakin1, Pavel Bakhvalovl2, Alexey Duben1,3, Andrey Gorobets1, Tatiana Kozubskaya1
    1Keldysh Institute of Applied Mathematics RAS, Moscow, Russia
    2Moscow Institute of Physics and Technology, Dolgoprudny, Moscow region, Russia
    3Moscow State Technological University STANKIN, Moscow, Russia
  • Numerical simulation expected acoustic characteristics aircraft cabin with new generation engines
    V.S. Baklanov
    "Tupolev", Moscow, Russia
  • Experience of CFD data implementation for preparation and performing the wind tunnel experiment with non-stationary separations and boundary layer laminar-turbulent transition taking into account
    S.M. Bosnyakov, V.V. Vlasenko, S.V. Matyash, S.V. Mikhaylov
    Central Aerohydrodynamic Institute, Zhukovskiy, Moscow region, Russia
  • Analysis of pressure data obtained in the near field of transonic jets using wavelet transform
    Roberto Camussi1, Silvano Grizzil2
    1Universita Roma Tre, Rome, Italy
    2CNR-INSEAN, , Italian Hydrodynamic Institute, Rome, Italy
  • Different approaches in correlation modeling of noise sources in turbulent jet
    S.A. Chernyshev, V.F. Kopiev
    Central Aerohydrodynamic Institute, Moscow Research Complex, Moscow, Russia
  • Advanced Engine Noise Control Based on Plasma Actuators (FP7 Project ORINOCO)
    Franck Clero1, Victor Kopiev2
    1ONERA, France
    2Central Aerohydrodynamic Institute, Moscow Research Complex, Moscow, Russia
  • Modelling of turbulent jet by CABARET method
    G.A. Faranosov1, V.M. Goloviznin1,2, S.A. Karabasov1,2,3, V.G. Kondakov1, V.F. Kopiev1, M.A. Zaitsev1,2
    1Moscow Institute of Nuclear Safety, Moscow, Russia
    2Central Aerohydrodynamic Institute, Moscow Research Complex, Moscow, Russia
    3University of Cambridge, Cambridge, UK
  • Aeroacoustics of supersonic boundary layers
    S.A. Gaponov
    Khristianovich Institute of Theoretical and Applied Mechanics of the Siberian Branch of the Russian Academy of Sciences, Novosibirsk, Russia
  • Sound generated by coherent structures in subsonic jets
    Andre V. Cavalieri1, Peter Jordan2, Yves Gervais2
    1Pprime Institute, Poitiers, France and InstitutoTecnologico de Aeronautica, Sao Jose dos Campos, Brazil
    2Pprime Institute, Poitiers, France
  • Aeroacoustics of transitional airfoils
    Vladimin Golubev1, Michel Roger2, Reda Mankbadi3
    1Embry-Riddle Aeronautical University, Daytona Beach, USA
    2Ecole Centrale de Lyon, Ecully, France
    3Embry-Riddle Aeronautical University, Daytona Beach, USA
  • Understanding and reduction of cruise jet noise at aircraft level
    Jerome Huber
    Engineer, AIAA member, Airbus Operations SAS, 316 route de Bayonne, 31060 Toulouse, France
  • Towards hybrid CAA with ground effects
    Marc C. Jacob1, Didier Dragna2, Adrien Cahuzac2, Jerome Boudet2, Philippe Blanc-Benon2
    1Laboratoire de Mecanique des Fluides et d’Acoustique, Universite Claude Bernard Lyon I / CNRS, Villeurbanne, France
    2Laboratoire de Mecanique des Fluides et d’Acoustique, Ecole Centrale de Lyon / CNRS, Ecully, France
  • An investigation of the mechanisms of sound generation in initially laminar, subsonic jets using the Goldstein acoustic analogy
    Sergey A. Karabasov1, Christophe Bogey2, Tom Hynes1
    1Whittle Laboratory, University of Cambridge Department of Engineering, Cam-bridge, CB3 0DY, UK
    2Laboratoire de Mecanique des Fluides et d’Acoustique, UMR CNRS 5509, Ecole Centrale de Lyon, Universite de Lyon, 69134 Ecully, France
  • Direct numerical simulation of supersonic boundary layer stabilization with ultrasonic absorptive porous coatings
    D.V. Khotyanovsky, A.N. Kudryavtsev
    Khristianovich Institute of Theoretical and Applied Mechanics of the Siberian Branch of the Russian Academy of Sciences, Novosibirsk, Russia
  • Direct control of instability waves in turbulent jet
    V.F. Kopiev, I.V. Belyaev, M.Yu. Zaitsev, V.A. Kopiev, G.A. Faranosov
    Central Aerohydrodynamic Institute, Moscow Research Complex, Moscow, Russia
  • Comparative accuracy assessment of contemporary shock capturing schemes in simulation of interaction of sound waves with shocks
    D.V. Khotyanovsky, A.N. Kudryavtsev
    Khristianovich Institute of Theoretical and Applied Mechanics of the Siberian Branch of the Russian Academy of Sciences, Novosibirsk, Russia
  • Large eddy simulation of the flow past a circular cylinder at Reynolds numbers 3900, 20000 and 140000
    Dmitry Lysenko1, Ivar Ertesvag2, Kjell Eric Rian1
    1Norwegian University of Science and Technology, Trondheim, Norway
    2Computational Industry Technologies AS, Trondheim, Norway
  • Slat noise measurement and numerical prediction in the VALIANT programme
    Eric Manoha1, Marc Terracol1, Benoît Lemoine2, Ingrid Le Griffon1, Thomas Le Garrec1
    1Office National d'Études et de Recherches Aérospatiales, Châtillon, France
    2Ecole Centrale de Lyon, Ecully, France
  • A multi-space-time algorithm for concurrent large/small scale fluid dynamics simulations
    Anton P. Markesteijn, Sergey A. Karabasov
    University of Cambridge, Cambridge, CB3 0DY, UK
  • Flow stability of isolated planar vortices
    I.S. Menshov
    M.V. Keldysh Institute of Applied Mathematics of RAS, Moscow, Russia
  • Flow around tandem cylinders and its noise emission with DDES and IDDES
    B. Greschner, D.Eschricht, C.Mockett, F.Thiele, U.Michel
    Technische Universitat Berlin, Germany
  • Efficient hybrid RANS-CAA method for prediction of single- and dual-stream jet mixing noise
    Andrej Neifeld, Roland Ewert
    Institute of Aerodynamics and Flow Technology, Technical Acoustics, German Aerospace Center (DLR), Braunschweig, Germany
  • Numerical investigations of tonal noise of counter rotating open rotors
    A.A. Rossikhin, I.A. Brailko, V.I. Mileshin
    CIAM, Moscow, Russia
  • CABARET scheme with conservation flux asynchronous timestepping for computational aeroacoustics
    V.A. Semiletov, Sergey A. Karabasov
    University of Cambridge, Cambridge, CB3 0DY, UK
  • BEM method initially based on FEM approximation
    J. Poblet-Puig1, A.V. Shanin2, V.Yu. Valyaev2
    1Universitat Politecnica de Catalunya (Barcelona, Spain), Laboratori de Calcul Numeric
    2M.V. Lomonosov Moscow State University, department of physics, Moscow, Russia
  • Using highly accurate multioperators-based optimized schemes for numerical simulation of sound generation due to instability of subsonic and supersonic jets
    A.I. Tolstykh, M.V. Lipavskii, D.A. Shirobokov
    Computing Center of RAS, Moscow, Russia