Chairpersons Jean Muylaert (ESTEC) David Hills (AIRBUS) Gorimir G. Chernyi (RAS) Mikhail S. Ivanov (ITAM) Session 2.1- Aerothermodynamic Phenomena I Tuesday Morning/ 5 July 2005  Chaired by D. Fletcher, VKI and A.Kolesnikov, IPM Tchaikovsky hall 2.01.02 9h00   Combined Approach for the Experimental Evaluation of the Heterogeneous Catalicity Parameters under Atmospheric Re.entry Conditions   M. Balat.Pichelin, L. Bedra, CNRS, Font.Romeu, FR         2.01.03 9h25   Predicting Catalytic Properties of SiC Material for the Pre.X Vehicle Re.Entry Conditions   A. Kolesnikov, A. Gordeev, S. Vasil'evskii, IPM, , Moscow, RU J..L. Vérant, ONERA, Toulouse, FR         2.01.04 9h50   Experimental and Theoretical Predictions of the Efficiency of Atomic Oxygen Recombination and Chemical Energy Accommodation on Space Vehicles Coatings   V..L. Kovalev, Moscow State University, Moscow, RU M. Balat.Pichelin, CNRS, Font.Romeu, FR A. Kolesnikov, RAS, Moscow, RU A. Krupnov, Moscow State Univ., RU         2.01.05 10h15   On Material Catalycity Effect on Heat Transfer to Hypersonic Vehicles in Multi.Component Gas Mixture   G. Zalogin, V. Vlasov, V. Lunev, TsNIIMash, Korolev, RU         2.01.06 10h40   Laminar Turbulent Transition in Hypersonic Boundary Layer and Its Control   A. Maslov, ITAM, Novosibirsk, RU         2.01.07 11h05   Experimental Investigation of a Boundary Layer Transition on Cones in a Hypersonic Flow on the Gasdynamic Facility of Superhigh Pressure A.1   M. Topchiyan, A. Vasil'ev, V. Rychkov, Lavrentyev Institute of Hydrodynamics, SB RAS, Novosibirsk, RU         2.01.08 11h30   Direct Numerical Simulation of Supersonic Boundary Layer Receptivity to Free.Stream Disturbances   I. Egorov, V. Soudakov, TsAGI, Zhukovsky, RU A. Fedorov, MIPT, Zhukovsky, RU Session 2.2 - Plasma Interaction and Flow Control Tuesday Morning/ 5 July 2005  Chaired by A. Gulhan, DLR and V. Bityurin, IVTAN Glinka hall 2.02.01 9h00    Some Problems of MHD Control in Hypersonic Flow   A. Vatazhin, O. Gouskov, M. Danilov, V. Kopchenov, CIAM, RU         2.02.02 9h25   High Speed Flow Control Using Pulsed Energy Deposition   D. Knight, H. Yan, RUTGERS, The State University of New Jersey, Piscataway, US G. Candler, R. Kandala, Univ. Minnesota, Minneapolis, US G. Elliott, N. Glumac, Univ. Illinois, Urbana, US A. Zheltovodov, E. Pimonov, Inst. of Theor. and Applied Mecha., Novosibirsk, RU         2.02.03 9h50   Research of Shock Wave.Induced Vortex Breakdown Control by Energy Deposition   A. Zheltovodov, Institute of Theoretical and Applied Mechanics, Novosibirsk, RU E. Pimonov, D..D. Knight, The State Univ.of New Jersey, Piscataway, US         2.02.04 10h15   Numerical Modelling of Corona Discharges and their Interaction with Aerodynamics   F. Thivet, J.-C. Matéo.Vélez, F. Rogier, G. Quinio, ONERA, Toulouse, FR P. Degond, MIP, Toulouse, FR         2.02.05 10h40   Active Flow Control by the Sliding Electric Arc Discharge   V. Golub, D. Blagodatskih, M. Bragin, V..V. Volodin, IHED, Moscow, RU . V..S. Aksenov, S..A. Gubin, MEPI, Moscow, RU . I..N. Laskin, CIAM, Moscow, RU         2.02.06 11h05   Aerodynamic Effects due to Electrical Discharges Generated Inflow   S. Leonov, K. Savelkin, D. Yarantsev, IVTAN, Moscow, RU V. Gromov, MSU, Moscow, RU         2.02.07 11h30   Boundary Layer Control by Gas Discharge Plasma   A. Starikovskii, D. Roupassov, I. Zavyalov, Moscow Instit. of Physics and Tech., RU . S. Saddoughi, GE G.R.C., Schenectady, NY, US         2.02.08 11h55   Hysteresis Effect and Stability Problem for the Front Separation Regions Control by the Localized Energy Deposition in the Upstream Flow   P..Y.Georgievsky, Moscow State University, RU V. Levin, IACP, Vladivostok, RU Session 2.3 - Experimental Facilities, Methods and Measurement Techniques I Tuesday Afternoon/ 5 July 2005  Chaired by T. Paulat, Dassault and V. Lapygin, TsNIIMash Tchaikovsky hall 2.03.01 14h00    Pulse Technique for In.Situ Flight Simulation and Working.off of Aerothermogasdynamic of Rockets and Reusable Transporting Space Systems    V. Kislykh, TsNIIMash, Korolev, RU         2.03.02 14h25   Real.Time Extraction of Critical Aerodynamic Flow Characteristics, Loads and Moments from Surface Signatures   S..M. Mangalam, Tao Systems, Hampton, US         2.03.03 14h50   Calibration Trials of Working Capabilities of the New Hypersonic Wind Tunnel AT.303 at ITAM   V. Zvegintsev, A. Kharitonov, N. Adamov, L. Vasenev, A. Kuraeva, D. Nalivajchenko, A. Novikov, S. Shpak, V. Chirkashenko, ITAM, Novosibirsk, RU         2.03.04 15h15   Flight and Experimental Facilities for Researching the Problems of the Advanced Flight Vehicles Creation   V. Grigoriev, A. Kondratov, P. Panteleev, S. Pernitsky, V. Tsyplakov, GFRI, Zhukovsky, RU A. Roudakov, V. Semenov, BCIAEM, Moscow, RU         2.03.05 15h40   Flow Conditions in the Plasma Wind Tunnels of the Laboratoire d'Aerothermique   J..C. Lengrand, V. Lago, CNRS, Orléans, FR P. Skovorodko, SBRA, Novosibirsk, RU I..A. Graur, IUSTI, Marseille, FR         2.03.06 16h05   Extended Capabilities of the IPG.4 Plasmatron in Supersonic Regimes for Re.Entry Simulation   A. Kolesnikov, A. Gordeev, A. Trukhanov, Inst. for Problems in Mech., Moscow, RU         2.03.07 16h30   A Ground to Flight Extrapolation Procedure for a Launcher Configuration   A. Nicoli, B. Imperatore, M. Marini, P. Catalano, CIRA, Capua, IT         2.03.08 16h55   P6.2 Cold Gas Test Facility for Simulation of Flight Conditions, Current Activities   K. Schafer, C. Bohm, H. Krommuller, R. Stark, H. Zimmermann, DLR, Hardthausen, DE Session 2.4 - CFD Simulation I Tuesday Afternoon/ 5 July 2005  Chaired by J.-P. Tribot, Dassault Aviation and Gromov, MSU Glinka hall 2.04.01 14h00   A Comparison of Different Numerical Approaches for Calculating a Martian Entry Flow   J..C. Lengrand, E. Chabut, CNRS, Orléans, FR M. Sokolova, Lomonosov MSU, Moscow, RU T. Elizarova, RAS, Moscow, RU         2.04.02 14h25   Aerothermodynamic Model of a Martian Descent Space Vehicles   S. Surzhikov, I. Sharikov, Institute for Problems in Mechanics Russian Academy of Sciences, Moscow, RU         2.04.03 14h50   CEDRE: Development and Validation of a Multiphysic Computational Software   B. Courbet, P. Chevalier, D. Dutoya, P. Klotz, E. Ruiz, J. Troyes, P. Villedieu, ONERA, Châtillon.Toulouse, FR         2.04.04 15h15   An Improvement of the Dual Time Stepping Technique for Unsteady RANS Computations   C. Marongiu, P..L. Vitagliano, P. Catalano, CIRA, Capua, IT V. Tarantino, D. Di Serafino, 2nd Univ. of Naples, Caserta, IT         2.04.05 15h40    Eulerian Monte Carlo Methods for Solving Joint Velocity.Scalar PDF Equations in Turbulent Reacting Flows    V. Sabel'nikov, O. Soulard, ONERA, Palaiseau, FR         2.04.07 16h30   The Level and Multi Temperature Models of Thermally Nonequilibrium Gas for Problems in High Speed Gas Flow   S. Losev, M. Pogosbekian, A. Sergievskaya, Moscow State University, RU         2.04.08 16h55   Numerical Simulations of the Flow Inside an S-Shaped Intake Diffuser   A.L. Vuillerme, S. Deck, ONERA, Châtillon, FR R. Chevrier, MBDA, FR Session 2.5 - CFD Simulation II Wednesday Morning/ 6 July 2005  Chaired by I. Egorov, TsAGI and W.Schroeder, RWTH Aachen Tchaikovsky hall 2.05.01 9h00    Large.Eddy Simulation of a Non.Isothermal Turbulent Jet and Wake Vortex Interaction    O. Labbé, ONERA, Châtillon, FR         2.05.02 9h25   Comparison of Modern Turbulence Models for Aero.Thermal Applications   A. Celic, G. Chevalier, C..A. Negulescu, CERFACS, Toulouse, FR         2.05.03 9h50   Vortex Control on Delta Wing with Rounded Leading Edges   D. Barberis, F. Renac, P. Molton, ONERA, Meudon, FR         2.05.04 10h15   Validation of an A.Priori Aerodynamic Model Based on CFD Results   W..G..M. Vos, J..M. Cnossen, H. Bijl, L..L..M. Veldhuis, Delft Univ. of Tech., NL         2.05.07 10h40   Large Eddy Simulation of the Flow Around a Slat in a High Lift Configuration   S. Ben Khelil, ONERA, Châtillon, FR         2.05.08 11h05   Numerical Approach to the Aeroacoustics of Complex Jet Flows : Methodology, Tests and Applications   M. Shur, Federal Scientific Center, St Petersburg, RU P..R. Spalart, Boeing Com. Airplanes, Seattle, US M. Strelets, NTS, St.Petersburg, RU Session 2.6 - Planetary Entry and Earth Reentry Aerothermodynamics Wednesday Morning/ 6 July 2005  Chaired by S. Borrelli, CIRA and V. Neiland, TSaGI Glinka hall 2.06.01 9h00    Preparing for reentry with EXPERT: The ESA in flight ATD Research programme    J..M. Muylaert, M. Caporicci, ESA/ESTEC, Noordwijk, NL         2.06.02 9h25   Aerodynamic of Reentry Spacecraft Clipper   A. Dyadkin, A. Krylov, A. Reshetin, Yu. Semenov, T. Simakova, V. Tokarev, SP Korolev RSC Energia, RU M. Kazakov, TsNIIMash, Korolev, RU         2.06.03 9h50   Aerocapture control problem for reentry vehicle of lifting body shape   V. Yaroshevsky, A. Bobylev, V. Kobzev, V. Poedinok, S. Suprunenko, CAI, Zhukovsky, RU A. Dyadkin, A. Reshetin, RSC Energia, Korolev, RU         2.06.04 10h15   Experimental Investigations of Aerodynamics of Reentry Vehicles at Natural Reynolds Number   A. Kharitonov, N.Adamov, V. Zvegintsev, M. Brodetsky, I. Mazhul, ITAM, Novosibirsk, RU J..C. Paulat, EADS.ST, Les Mureaux, FR J..M. Myulaert, W. Kordulla, ESTEC, Noordwijk, NL         2.06.05 10h40   Pre.X Supersonic Regime; Experimental and CFD Analysis   J..P. Tribot, M. Stojanowski, Dassault Aviation, St.Cloud, FR J. Oswald, CNES, Evry, FR         2.06.06 11h05   Computational Analysis of ATV Re-Entry Flow and Explosion Assessment   R. Schmehl, Ph. Reynier, AOES-Leiden, NL D..E. Boutamine, J. Steelant, L. Marraffa, ESA/ESTEC, Noordwijk, NL         2.06.07 11h30   Navier Stokes Computations for Space Vehicles of Martian Return Sample Mission   V. Gromov, N. Afonina, V. Sakharov, Moscow State Univ., RU         2.06.08 11h55   Review of Experimental and Numerical ATD Analysis of Mars PREMIER MSRO Vehicle   J..L. Verant, J. Soutadé, J. Hylkema, ONERA, Toulouse, FR M. Spel, W. Dieudonné, R. Tech., FR Session 2.7 - Aerothermodynamic Phenomena II Wednesday Afternoon/ 6 July 2005  Chaired by J.M. Charbonnier, CNES and A. Kharitonov, ITAM Tchaikovsky hall 2.07.01 14h00    Review of ITAM Experiments on Shock/Vortex Interactions    A. Shevchenko, I. Kavun, A. Pavlov, V. Zapryagaev, ITAM, Novosibirsk, RU         2.07.02 14h25   Investigation of Vortex Flow with Shock Wave   V. Zudov, ITAM, Novosibirsk, RU         2.07.03 14h50   Investigation of Compressible Mixing Layer Affected by Artificial Acoustic Disturbances   V. Lebiga, V. Zinoviev, A. Pak, ITAM, Novosibirsk, RU         2.07.04 15h15   Extrapolation to Flight of Aerodynamic Heating Measurements and Determination of In.Flight Radiation Equilibrium Surface Temperature in Hypersonic / High Enthalpy Flow Conditions   G..A. Simeonides, Hellenic Aerospace Industry, Schimatari, GR         2.07.05 15h40   Analysis of the Kinetic Processes in Dusty Plasma Forming in the Hypersonic Flow over the Vehicle Crossing the Upper Atmosphere   A. Savel'ev, A. Starik, N. Titova, CIAM, Moscow, RU S. Losev, MSU, RU         2.07.06 16h05   Radiating Heat Transfer at the Entrance of Space Bodies to the Earth's Atmosphere   V. Stulov, Moscow State University, RU         2.07.07 16h30   Measurements and Analysis of UV.Radiation Intensity of Plasma Structure Along Orbital Re.Entry Trajectory of Space Vehicle "SOYUZ.TM" Based on Observation Data Obtained on Board ISS   Yu. Plastinin, B. Zemliansky, G. Karabadzhak, A. Gorshkov, V. Vlasov, B. Khmelinin, R. Kovalev, G. Sipatchev, G. Zalogin , TSNIIMash, Korolev, RU Session 2.8 - Configuration Aerodynamics and Optimisation Wednesday Afternoon/ 6 July 2005  Chaired by O. Bas, NLR and A. Kraiko, CIAM Glinka hall 2.08.01 14h00   Optimal Control in Gas Dynamic: Methods and Results   A.N. Kraiko, CIAM, Moscow, RU         2.08.02 14h25    An Economical and Accurate Modelling of Aircraft Aerodynamics    M. Zamurad Shah, A. Mughal, Nat. Engineering and Scien. Commission, Islamabad, PK         2.08.03 14h50   Multi-Objective Optimization of 3D Turbomachinery Blades   S. Pierret, Cenaero, Gosselies, BE         2.08.04 15h15   Coupled Thermal/Aerothermal Simulations of Engine Compartments   A. Massol, O. Verseux, M.-J. Esteve, AIRBUS France, Toulouse, FR         2.08.07 15h40   Wings and Fighter Aircraft Flow Computations Using Implicit WENO Euler / Navier-Stokes Solvers   J.-Y. Yang, Y.-C. Perng, J.-C. Huang - Inst. of Applied Mechanics, Taipei, TW         2.08.08 16h05   Modeling of Nonstationary Flow in a Variable Cross Section Flat Duct at a Distributed Pulse Periodical Energy Supply   A. Latypov, ITAM, Novosibirsk, RU Session 2.9 - Unsteady Flows Thursday Morning/ 7 July 2005  Chaired by J.-J. Philippe, ONERA and Guvernyuk, MSU Tchaikovsky hall 2.09.01 9h00    Modelling of the Effect of the Inlet Turbulence Parameters on Unsteady Flows and Heat Transfer    V. Aleksin, Institute for Problems in Mechanics, Moscow, RU         2.09.02 9h25   Predicting the Onset of Flow Unsteadiness Based on Stability Analysis   D. Magidov, A. Garbaruk, Saint Petersburg State Polytechnic University, RU J..D. Crouch, B.C.A., Seattle, US         2.09.03 9h50   Control Effectiveness of Exhaust Jet with a Wing Body Configuration   F. F. Lopez Parra, K. Kontis, Univ. Manchester, GB         2.09.04 10h15   Investigation of an Oscillating Airfoil by Means of Composed Optical Records Technique   J. Ulrych, T. Jelinek, Dpt. Of High Speed Aerodynamics, Praha, CZ         2.09.05 10h40   A Framework for Accurate and Efficient CFD Analysis of Helicopter Rotors   R. Steijl, G..N. Baakos, K..J. Badcock, Univ. of Glasgow, GB         2.09.06 11h05   Modification of Wall Boundary Conditions for Low Re k.omega Turbulence Models Aimed at Grid Sensitivity Reduction   E. Smirnov, D. Zaitsev, Saint Petersburg State University, RU         2.09.07 11h30   A Scalable Wall Function Approach for High Reynolds Number Flows   P. Catalano, P..L. Vitagliano, CIRA, Capua, IT         2.09.08 11h55   Mathematical Modeling of Aircraft Unsteady Aerodynamics at High Angles of Attack in the Problems of Flight Dynamics   A. Khrabrov, TsAGI, Zhukovsky, RU Session 2.10 - High Altitude Aerodynamics Thursday Morning/ 7 July 2005  Chaired J. Reese, University of Strathclyde and M. Ivanov, ITAM Glinka hall 2.10.01 9h00   High.Altitude Aerothermodynamics of Space Vehicles   M. Ivanov, Institute of Theorical and Applied Mechanics, Novosibirsk, RU         2.10.02 9h25   Modelling of Processes of External Contamination of Space Vehicles by Orientation Thrusters Jets in Vacuum Chambers   V. Yarygin, V. Prikhodko, I. Yarygin, Kutateladze Instit. of Thermophysics, Novosibirsk, RU Yu. Gerasimov, A. Krylov, Korolev Rocket and Space Corp. "Energia", RU         2.10.03 9h50   Some Consequences of Non.Local Equilibrium in Hypersonic Aerodynamic Flows   J..M. Reese, C..J. Greenshields, Univ. of Strathclyde, Glasgow, UK         2.10.04 10h15   Numerical Investigation of Causes of Spacecraft Surface Contamination in Operation of Control Thruster   A. Schmidt, Yu. Golovachov, E. Kumzerova, B. Reznikov, IOFFE Institute, St Petersburg, RU D. Khotyanovsky, A. Kudryavtsev, ITAM, RU         2.10.05 10h40    Mathematical Modeling of Spacecraft Charging at Operation of Onboard Plasma Thrusters    L. Novikov, V. Mileev, K. Krupnikov, MSU, RU V. Malko, A. Plokhih, MAI, Moscow, RU         2.10.06 11h05   Hypersonic Flow Models in Astrophysics and Applied Physics   J..P. Lafon, Observatoire de Paris . GEPI, Meudon, FR         2.10.07 11h30   Rarefied Gas Flow Around Rough Bodies   M. Anolik, Saint Petersburg State University, RU         2.10.08 11h55   Simulation of Space Vehicle System Elements Separation at Supersonic Velocities   V. Eremin, V. Skripnyak, P. Kuznetsov, TsNIIMash, Korolev, RU Session 2.11 - Experimental Facilities, Methods and Measurement Techniques II Thursday Afternoon/7 July 2005  Chaired by M. Auweter-Kurz, U. Stuttgart and Rukavets, TsAGI Tchaikovsky hall 2.11.01 14h00   Design of the In.Flight Sensor Systems PYREX, PHLUX and RESPECT for the European Capsule EXPERT   G. Herdrich, M. Auweter.Kurtz, M. Fertig, S. Löhle, S. Pidan, M. Winter, Univ. of Stuttgart, DE         2.11.02 14h25   Features of Processing of Ablating Calorimeter Type Gauges Indications   E. Gubanov, TsNIIMash, Korolev, RU         2.11.03 14h50   Increasing Power of High Enthalpy Short Duration Wind Tunnels for Investigations at Mach Numbers M=4.7   V. Shumsky, M. Yaroslavtsev, ITAM, Novosibirsk, RU         2.11.04 15h15   Automation of Thermal Paints Analysis for Temperature Measurement of Engine Components   R. Andral, C. Lempereur, H. Buchet, ONERA, Toulouse, FR J..Y. Prudhomme, Turbomeca, Bordes, FR         2.11.05 15h40   Dynamic Method Used for Determining the Aerodynamic Forces Effecting the Models Tested in Short Duration Wind Tunnel   A. Latypov, ITAM, Novosibirsk, RU         2.11.06 16h05    Studying of the Shock Wave Effect on the Heat Transfer in the Near Wall Flow of a Channel    V. Zinoviev, V. Lebiga, A. Pak, V. Trofimov, ITAM, Novosibirsk, RU         2.11.07 16h30   Experimental Study of Separated Flow on Unswept Wings with Smooth and Wavy Surface at Small Reynolds Numberss   V. Kozlov, B. Zanin, I. Zverkov, ITAM, Novosibirsk, RU         2.11.08 16h55   Hot Wire Visualizations of Breakdown to Turbulence in Complex Flows   V..G. Chernoray, L. Lofdahl, Chalmers University of Technology, Gothenburg, SE V. Kozlov, ITAM, Novosibirsk, RU P. Pratt, SAE, Belfast, GB >> Inter-Symposium 2-5 Session:       Flight physics for aircraft and launch vehicles including reentry bodies-Propulsion Physics Session 2.12-5.14 - Nozzle Flow Separation and Buffeting Thursday Afternoon/ 7 July 2005  Chaired by P. Reijasse, ONERA and Vorozhtsov Glinka hall 5.14.01 14h00    Buffeting on the AFT Body of ARIANE 5: Interaction Between System and Subsystem in the Qualification Process   F. Ravary, V. Le Gallo, S. Radulovic, EADS Space, Les Mureaux, FR         5.14.02 14h25   Numerical Investigation of the Buffet Phenomenon with URANS Equations    V. Brunet, ONERA, Châtillon, FR         5.14.03 14h50   Simulation of the ARIANE 5 Nozzle Section by DES   H. Lüdeke, DLR, Braunschweig, DE         5.14.04 15h15   Flow Separation Regimes Induced by Cap.Shock in Over.Expanded Optimized Propulsive Nozzles   Ph. Reijasse, R. Poutrel, ONERA, Meudon, FR         5.14.05 15h40   Flow Structures and Separation in Overexpanded Rocket Nozzles   F. Nasuti, M. Onofri, Univ.of Roma "La Sapienza", IT         5.14.06 16h05   Cold Flow Testing of Dual Bell Nozzles in Altitude Simulation Chambers   R. Stark, Ch. Böhm, O. Haidn, H. Zimmermann, DLR, Hardthausen, DE