Monday, July 12, 2004
8:30 – 9:30
Invited Lecture, Harbour A & B
Topics in Detached-Eddy Simulation
Dr. Philippe Spalart
Boeing Commercial Airplanes, USA
9:30 – 10:00
10:00 – 12:00
Coffee Break, Harbour Foyer
Session 1, Harbour A
Session 2, Harbour B
Session 3, Harbour C
Applications I
Modelling and Simulation of
Turbulence I
Multifluid and Multiphase
Flows I
Chair: Philippe Spalart
Chair: Remi Abgrall
Calculation of Static and Dynamic
Stability Derivatives of the F/A-18E in
Abrupt Wing Stall Using RANS and
DES
Lattice Boltzmann Simulations in
Chemical Engineering
Forsythe, J. R., Fremaux C. M.,
Hall, R. M.
Cobalt Solutions, LLC
NASA Langley Research Center
USA
University of Duisberg-Essen
Germany
Large Eddy Simulation of Flow
Around a Slat with a Blunt Trailing
Edge
A Scheme for Compressible TwoPhase Flow and Interface Problems
Chair: Barry Koren
10:00 – 10:30
Transonic Flows of BZT Fluids
Through Turbine Cascades
Cinnella, P., Congedo, P. M.,
Laforgia, D.
University of Lecce
Italy
10:30 – 11:00
CFD Simulations of the Space
Shuttle Launch Vehicle with Booster
Separation Motor and Reaction
Control System Plumes
Hänel, D., Lantermann, U.
Abgrall, R., Papin, M., Hallo, L.
Khelil, S. B.
11:00 – 11:30
Gea, L. M., Vicker, D.
The Boeing Company
NASA Johnson Space Center
USA
ONERA
France
An Efficient Numerical Method for
3D Viscous Ship Hydrodynamics
with Free-Surface Gravity Waves
Implicit Large Eddy Simulation of a
Flow around a Subsonic Airfoil near
its Stall Angle
A New Accurate Method for Simulating
Polydispersed Two-Phase Flows
Koren, B., Lewis, M.
Komurasaki, S., Kuwahara, K.
Nihon University
Institute of Space and Astronautical
Science
Japan
Dufour, G., Massot, M., Villedieu, P.
Numerical Approach to the Analysis
of Internal Pressure of M-V Rocket
Fairing
DNS of compressible turbulent
boundary layer over a blunt wedge
The Characteristics-Based Matching
Method (CBM) for High-Speed
Multiphase Fluid-Fluid Flows
Yamamoto, A., Fujimoto, K., Fujii, K.,
Tsuboi, N.
Okanomizu University
University of Tokyo
Li, X., Fu, D.
Nourgaliev, R. R., Liou, M. -S.,
Dinh, T. N., Theofanous, T. G.
CWI
Netherlands
11:30 – 12:00
LNM, Institute of Mechanics, CAS
China
Japan Aerospace Exploration Agency
Japan
12:00 – 1:30
Lunch, Pier 4 & 5
Université Bordeau
CEA CESTA
France
ONERA/DMAE-2
Universite Claude Bernard
France
University of California, Santa Barbara
NASA Glenn Research Center
USA
Monday, July 12, 2004
1:30 – 3:30
1:30 – 2:00
Session 4, Harbour A
Session 5, Harbour B
Session 6, Harbour C
Algorithms I
Parallel Algorithms I
Magnetohydrodynamics
Chair: Marian Nemec
Chair: Clinton Groth
Chair: Joe Shang
A Matrix-Free Implicit Method for
Flows at All Speeds
Parallel Simulation for Strong Blast
Wave from TNT Explosion on LargeScale PC-Cluster
A Central, Diamond-Staggered Dual
Cell, Finite Volume Method for Ideal
Magnetohydrodynamics
Aoki, T., Kato, K., Saburi, T.,
Yoshida, M.
Tokyo Institute of Technology
National Institute of Advance
Industrial Science and Technology
Japan
Arminjon, P., Touma, R.
An Efficient and Accurate PressureCorrection Method for all Mach
Numbers
A Parallel Implicit Adaptive Mesh
Refinement Algorithm Algorithm for
Body-Fitted Multi-Block Mesh
Simulation of Supersonic Flows in
Inductively Coupled Plasma Tunnels
Nerinckx, K., Vierendeels, J.,
Dick, E.
Groth, C. P. T.
Beccantini, A., Corre, C., Kloczko, T.
CEA Saclay / DM2S / LTMF
SINUMEF Lab, ENSAM
France
2:00 – 2:30
Ghent University
Belgium
2:30 – 3:00
The Analysis of Electromagnetic
Wave Using CIP Scheme with
Soroban Grid
Ogata, Y., Yabe, T., Takizawa, K.,
Ohkubo, T
Tokyo Institute of Technology
Japan
3:00 – 3:30
3:30 – 4:00
Canada
Diebel, J. R., Magin, T. E.,
Abeele, D. V., Degrez, G.
University of Toronto
Canada
von Karman Institute for Fluid
Dynamics
Belgium
MPI Parallelization of Unstructured
Mesh Adaption
Magneto- Fluid-Dynamics Interaction
Lepage, C. Y., St-Cyr, A.,
Habashi, W. G.
Newmerical Technologies
International, Canada
National Center for Atmospheric
Research, USA
McGill University, Canada
Shang, J. S., Surzhikov, S. T.
Multigrid Third-Order Least-Squares Parallel Implementation of a Dynamic
Solution of Cauchy-Riemann
Overset Unstructured Grid Approach
Equations on Unstructured
Triangular Grids
Madrane, A., Stuermer, A.,
Raichle, A.
Nishikawa, H.
German Aerospace Center
University of Michigan
Germany
USA
Coffee Break, Harbour Foyer
Wright State University, USA
Russian Academy of Science, Russia
Monday, July 12, 2004
4:00 – 5:30
Session 7, Harbour A
Session 8, Harbour B
Session 9, Harbour C
High-Order Schemes I
Modelling and Simulation of
Turbulence II
Upwind Schemes I
Chair: Alain Lerat
Chair: Jean-Yves Trepanier
Chair: Martin Peeters
4:00 – 4:30
High Order Residual-Based
Compact Scheme
Computation of the Turbulent
Boundary Layer on a Long Circular
Cylinder in Axial Flow with a Vorticity
Boundary Condition
An Upwind Moment Scheme for
Conservation Laws
Corre, C., Lerat, A.
Huynh, H. T.
Woods, M., Bull, M.
SINUMEF Lab, ENSAM
France
4:30 – 5:00
How Effective Are High-Order
Approximations in Shock-Capturing
Methods? Is There a Law of
Diminishing Returns?
NASA Glenn Research Center
USA
University of Adelaide
Australia
3D Fluid Flow around a Sphere at
Moderate Reynolds Numbers
Accurate and Efficient Re-evaluation of
Cell-interface Convective Fluxes
Matyushin, P. V., Gushchin, V. A.
Kim, K.-H., Kim, S.-S., Kim, C.
Russian Academy of Sciences
Russia
Seoul National University
Korea
Rider, W. J., Kamm, J. R.
Los Alamos National Laboratory
USA
5:00 – 5:30
Low Dissipative High Order
Schemes For 3-D Non-Ideal MHD
Computation of the Flow Around a Bluff
Body by Multi-Directional Finite
Difference Method
Yee, H., Sjögreen, B.
Lee, M. Y., Kawamura, T., Kuwahara, K.
Ochanomizu University
The Institute of Space and Astronautical
Science
NASA Ames Research Center, USA
The Royal Institute of Technology,
Sweden
5:30 – 6:30
Japan
Poster Session I, Harbour Foyer
3D Prediction of Developing
Numerical Simulation of Steady
Turbulent Flow in a 90 Curved Duct Newtonian and Non-Newtonian Flow
Using Linear and Non-Linear Low-Re
Through Vascular Stenoses
k-Models
Behrens, G. R., Agarwal, R.
Alemi, H., Raisee, M.
Washington University
University of Tehran
USA
Iran
Parallel 2D/3D Unsteady
Incompressible Viscous Flow
Computations Using an Unstructured
CFD Code
Adaptive Bounds to Outputs of the
Three Dimensional Steady
Incompressible Navier-Stokes
Equations
Chen, H., Huang, P. G.,
LeBeau, R. P.
Choi, H.–W., Paraschivoiu, M.
University of Kentucky
USA
University of Toronto
Concordia University
Canada
Finite Volume Methods for Fluid Flow
through Elastic Tubes
Brandner, M.
University of West Bohemia
Czech Republic
A Comparative Study of Three
Composite Schemes: LaxWendroff/Lax-Friedrichs, MacCormack/Lax-Friedrichs & MacCormack/Corrected Lax-Friedrichs
Schemes, Based on Conservation
Laws
Dauhoo, M. Z., Appadu, A. R.
University of Mauritius
Mauritius
Sails Aerodynamics: Evaluation of
Reynolds Number Effect on the CFD
Simulation of Downwind Sails and
Comparison with Experimental Data
Assessment of the Immersed
Boundary Technique for
Compressible CFD codes
Spectral Solution of High Speed Flow
over Blunt Bodies with Improved
Boundary Treatment
Delussu, G., Erriu, N., Mulas, M.,
Talice, M.
Delussu, G., Mulas, M., Talice, M.
Esfahanian, V., Boroomand, M.,
Najafi, M.
Center of Advanced Studies,
Research and Development in
Sardinia
Sardinia
Verification of Mathematical Model of
the Shock Wave/Dust Layer
Interaction Problem
Center of Advanced Studies,
Research and Development in
Sardinia
Sardinia
Automation of Unstructured Mesh
Generation for Objects in Direct
Contact for Store Release
Computations
Fedorov, A. V., Fedorova, N. N.,
Fedorchenko, I. A.
Fortin, F., Zoric, T.
Institute of Theoretical and Applied
Mechanics SD RAS
Russia
National Research Council (NRC)
Carleton University
Canada
Univerisity of Theoretical and Applied
Mechanics
Iran
Tuesday, July 13, 2004
8:30 – 9:30
Invited Lecture, Harbour A & B
High-End Computing Challenges in Aerospace Design and Engineering
F. Ronald Bailey
Advanced Management Technology Inc., NASA Ames Research Center, USA
9:30 – 10:00
10:00 – 12:00
Coffee Break, Harbour Foyer
Session 10, Harbour A
Session 11, Harbour B
Session 12, Harbour C
Optimization I
Modelling and Simulation of
Turbulence III
Applications II
Chair: Dimitri Mavriplis
Chair: Ron Bailey
Chair: Paola Cinnella
10:00 – 10:30
Surface Mesh Movement for
Aerodynamic Design of BodyInstallation Junction
Automated Euler and Navier-Stokes
Database Generation for a Glide-Back
Booster
Kim, H. -J., Nakahashi, K.
Chaderjian, N. M., Rogers, S. E.,
Aftosmis, M. J., Pandya, S. A.
NASA Ames Research Center
ELORET
USA
Tohoku University
Japan
10:30 – 11:00
11:00 – 11:30
Formulation and Multigrid Solution of
the Discrete Adjoint Problem on
Unstructured Meshes
LES of Combined Forced and
Natural Turbulent Convection in a
Vertical Slot
Numerical Simulation of Radiative
Heating for Atmospheric Reentry in
Martian Atmosphere
Mavriplis, D. J.
Yin, J., Bergstrom, D. J.
Rouzaud, O., Hylkema, J., Tessé, L.,
Vérant, J. -L.
University of Wyoming
USA
University of Saskatchewan
Canada
Aerodynamic Design of Transonic
Cascade Using Parallel
Computations of Global Optimizers
and Artificial Neural Networks
Numerical Study on k-w Turbulence
Models for Supersonic Impinging Jet
Flow Field
ONERA
France
An Implicit Preconditionned JFNK
Method for Fully Coupled Radiating
Flows. Application to Superorbital Reentry Simulations
Kim, E., Park, S. H., Kwon, J. H.
Mengistu, T., Ghaly, W.
Concordia University
Canada
11:30 – 12:00
An Analysis of Bodies Having
Minimum Pressure Drag in
Supersonic Flow: Exploring the
Nonlinear Domain
Turpault, R.
Korea Advanced Institute of Science
and Technology
Korea
Comparative Study of Reynolds
Stress Turbulence Models in FreeShear and Wall-Bounded Flows
Viti, V., Huang, P. G., Bradshaw, P.
University Bordeaux
France
Part of subsequent Flow Control
session:
Two- and Three-dimensional Flow
Optimization in Chemical Engineering
Palaniappan, K., Jameson, A.
Stanford University
USA
(see also paper at 1:30)
12:00 – 1:30
University of Kentucky
Stanford University
USA
Lunch, Pier 4 & 5
Bärwolff, G.
Technische Universität Berlin
Germany
Tuesday, July 13, 2004
1:30 – 3:30
Session 13, Harbour A
Session 14, Harbour B
Session 15, Harbour C
High-Order Schemes II
Adaptive Meshing
Flow Control
Chair: Virginie Daru
Chair: Kazuhiro Nakahashi
Chair: Chris Rumsey
(see also paper above at 11:30)
1:30 – 2:00
(continued from previous session)
An Error Indicator for Semidiscrete
Schemes
A NURBS-Based Shape
Optimisation Method for Hydraulic
Turbine Stay Vane
Numerical Simulation and Control of
Bluff-Body Flows Using the
Penalization Method
Marobin, D., Puppo, G.
Bruneau, C. H., Mortazavi, I.,
Wilczyk, G.
Poueymirou, D., Tribes, C.,
Trépanier, J.-Y.
Politecnico di Torino
Italy
Université Bordeau
France
École Polytechnique de Montréal
Canada
2:00 – 2:30
Super Compact Spatial Differencing
for the Linear and Nonlinear
Geophysical Fluid Dynamics
Problems
A Mesh Adjustment Scheme for
Embedded Boundaries
Application of Genetic Algorithm to
Two-Jet Control System on NACA
0012 Airfoil
Esfahanian, V., Ghader, S.
University of Tehran
Atmospheric Science &
Meteorological Research Center
Iran
University of Toronto
Canada
A New Discretization Method of
Governing Equations for High Order
Accuracy
Numerical Simulations of Flows Past
2D Complex Shapes Using Building
Cube Method (BCM)
Reynolds-Averaged Navier-Stokes
Computations of a Synthetic Jet in a
Turbulent Boundary Layer
Kim, D., Kwon, J. H.
Kitamura, S.
Rumsey, C. L.
Korea Advanced Institute of Science
and Technology
Korea
Institute of Computational Fluid
Dynamics
Japan
NASA Langley Research Center
USA
A High-Order Accurate Unstructured
GMRES Solver for the Compressible
Euler Equations
High-Density Mesh Flow
Computations by Building-Cube
Method
Active Control of Shock/Boundary
Layer Interaction in Transonic Flow
over Airfoils
Nejat, A., Ollivier-Gooch, C.
Nakahashi, K., Kim, L. -S.
Vadillo, J., Agarwal, R. K.
University of British Columbia
Canada
Tohoku University
Japan
(see also paper at 4:00)
Washington University in St. Louis
USA
Sachdev, J. S., Groth, C. P. T.
Huang, L., LeBeau, R. P., Hauser, T.
2:30 – 3:00
3:00 – 3:30
3:30 – 4:00
Coffee Break, Harbour Foyer
University of Kentucky
Utah State University
USA
Tuesday, July 13, 2004
4:00 – 5:30
Session 16, Harbour A
Session 17, Harbour B
Session 18, Harbour C
Multifluid and Multiphase
Flows II
Incompressible Flow
Upwind Schemes II
Chair: Dochan Kwak
Chair: Eric Laurendeau
(continued from previous session)
A One Point Shock Capturing Kinetic
Scheme for Hyperbolic Conservation
Laws
Chair: Meng-Sing Liou
4:00 – 4:30
Simulation of Multifluid Multiphase
Flows with AUSM+-up Scheme
Chang, C. -H., Liou, M. -S.
NASA Glenn Research Center
USA
Accurate Solution of Corner
Singularities in Axisymmetric and
Plane Flows Using Adjusted Mesh of
Finite Elements
Chandar, D. D. J., Rao, S. V. R.,
Deshpande, S. M.
Burda, P., Novotny, J., Sistek, J.
Czech University of Technology
Czech Republic
4:30 – 5:00
Computational Simulation of
Complex Fluid Physics Applications
Li, D., Xia, G., Venkateswaran, S.,
Merkle C. L.
Purdue University
USA
5:00 – 5:30
A Novel Physical Model and
Computational Method for NonIsotropic, Compressible Two-Fluid
Flow
Wackers, J., Koren, B.
Sensitivity Analysis of TimeDependent Incompressible Laminar
Flows
Accurate and Efficient Multidimensional TVD Interpolation
Kim, K.-H., Kim, S.-H., Kim, C.
Hristova, H., Etienne, S.,
Pelletier, D., Borggaard, J.
École Polytechnique de Montréal,
Canada
Virginia Tech, USA
Seoul National University
Korea
Comparison of Artificial
Compressibility Methods
On the Origin of the Carbuncle
Phenomenon
Kiris, C., Housman, J., Kwak, D.
Moschetta, J. -M., Chauvat, Y.,
Greissier, J.
Ecole Nationale Supérieure de
l’Aéronautique et de l’Espace
ONERA
France
NASA Ames Research Center
USA
CWI
Netherlands
5:30 – 6:30
Indian Institute of Science
India
Poster Session II, Pier 2 & 3
Complex Flow Patterns in Realistic
Geometry of Human Aorta
Interplay Between Inertia and Gravity
in Steady and Transient Thin-Jet Flow
Numerical Modeling of Leukocyte
Aspiration to Determine Cytoplasmic
Viscosity
Gardhagen, R., Svensson, J.,
Karlsson, M.
German, R., Khayat, R. E.
Golpaygan, A., Ashgriz, N.
Linkoping University
Sweden
University of Western Ontario
Canada
University of Toronto
Canada
Gradient Computation for Variational
Assimilation of Meteorological
Observations
3-D Heat and Fluid Flow Analysis of
Successively Variable Louver Angle
of Louver Fin Geometry in Compact
Heat Exchangers
Numerical Simulations of Free Surface
Flows with a Front Tracking Method
Horibata, Y.
Hsieh, C. T., Jang, J. Y.
Hosei University
Japan
National Cheng Kung University
Taiwan
Ji, H., Lien, F.-S., Strong, A. B.
University of Waterloo
Canada
Concept Study of Vortex Generators
for Simulation of Aircraft Wing-Tip
Vortices
Numerical and Experimental
Investigation of Two-Fluid Conjugate
Natural Convection in Panel Heat
Exchangers for Electric Transformers
Jiang, L. Y., Lee, B. H. K.
National Research Council (NRC)
Canada
Pattern Formation in Viscoelastic
Thermal Convection
Li, Z., Khayat, R. E.
Kurbatskii, K. A., Tahir, R.,
Brescasin, L., Stauder, F.
University of Western Ontario
Canada
Unifin International Inc.
Canada
Turbulent Transport of Passive Scalar The Simulation of Three-Dimensional Mass Transpiration Cooling Analysis at
Emitted from Line Source in an Open Intake Flows Using a Navier-Stokes Hypersonic Mach Numbers Using CFD
Flow
Solver
Tools
Liu, C.-H., Leung, D. Y. C.
Liu, J. J.
The University of Hong Kong
China
Chinese Academy of Sciences
China
Kulkarni, P. S., Kulkarni, V. N.,
Reddy, K. P. J., Saito, T.,
Takayama, K.
Indian Institute of Science, India
Tohoku University, Japan
Wednesday, July 14, 2004
8:30 – 9:30
Invited Lecture, Harbour A & B
Control of Shocks
Prof. Olivier Pironneau
Laboratoire Jacques-Louis Lions, University of Paris VI, France
9:30 – 10:00
10:00 – 12:00
Coffee Break, Harbour Foyer
Session 19, Harbour A
Session 20, Harbour B
Session 21, Harbour C
Optimization II
Algorithms II
Chair: Olivier Pironneau
Chair: Mohamed Hafez
Multifluid and Multiphase
Flows III
Chair: Sankaran Venkateswaran
10:00 – 10:30
Optimum Multidisciplinary and MultiA Low Dissipative Relaxation
Objective Wing Design in CFD Using Scheme for Hyperbolic Conservation
Evolutionary Techniques
Laws
Modeling Turbulent Interfacial Flows
Jafari, A., Ashgriz, N.
Gonzalez, L. F., Whitney, E. J.,
Srinivas, K., Périaux, J.
University of Sydney, Australia
Dassault Aviation, France
10:30 – 11:00
Advances in Aerodynamic Shape
Optimization
Kaushik, K. N., Rao, S. V. R.
Indian Institute of Science
India
University of Toronto
Canada
Solution of the Fluid Dynamical
Formulation of Nonlinear
Schrödinger Equation with Radial
Basis Function Interpolation
On Modeling of Collisions in Direct
Numerical Simulation of High-Speed
Multiphase Fluid-Solid (Particulate)
Flows
Hsieh, T. Y., Huang, J. C.,
Yang, J. Y.
Nourgaliev, R. R., Dinh, T. N.,
Theofanous, T. G.
National Taiwan University
Taiwan
University of California, Santa Barbara
USA
On the Use of CAD and Cartesian
Methods for Aerodynamic
Optimization
High Resolution Scheme for
Quantum Hydrodynamic Based on
Nonlinear Schrödinger Equation
A Second-Order Adaptive SharpInterface Method for Incompressible
Multiphase Flow
Nemec, M., Aftosmis, M. J.,
Pulliam, T. H.
Yang, J. Y., Huang, J. C.,
Hsieh, T. Y.
Sussman, M., Hussaini, M. Y.,
Smith, K. M., Zhi-Wei, R.
NASA Ames Research Center
USA
National Taiwan University
Taiwan
Florida State University
USA
Improvement of the Optimization
Method of the TSTO Configuration –
Application of Accurate
Aerodynamics
Multigrid Acceleration for Transonic
Aerodynamic Flow Simulations
Based on a Hierarchical Formulation
Large-Scale Direct Simulation of TwoPhase Flow Structure around a Spacer
in a Tight-Lattice Nuclear Fuel Bundle
Hafez, M., Wahba, E.
Takase, K., Yoshida, H., Ose, Y.,
Tamai, H., Akimoto, H.
Japan Atomic Energy Research
Institute
Yamato System Engineer
Japan
Jameson, A.
Stanford University
USA
11:00 – 11:30
11:30 – 12:00
Shimoyama, K., Fujii, K.,
Kobayashi, H.
University of Tokyo
University of California, Davis
USA
Japan Aerospace Exploration Agency
Japan
5:30 – 9:00
Dinner Cruise
Thursday, July 15, 2004
8:30 – 9:30
Invited Lecture, Harbour A & B
Multiscale Models of the Circulatory System
Prof. Alfio Quarteroni
Ecole Polytechnique Federale de Lausanne, Switzerland & Politecnico of Milan, Italy
9:30 – 10:00
10:00 – 12:00
Coffee Break, Harbour Foyer
Session 22, Harbour A
Session 23, Harbour B
Session 24, Harbour C
Algorithms for Unsteady
Flows
Applications III
Biological Flows
Chair: Jean-Jacques Chattot
Chair: Alfio Quarteroni
Numerical Simulation of the Shock
Wave – Boundary Layer Interaction
in a Shock Tube by Using a High
Resolution Monotonicity-Preserving
Scheme
Towards the 'In Vivo' computational
Hemodynamics
Chair: Michele Napolitano
10:00 – 10:30
A Third-Order-Accurate
Multidimensional ResidualDistribution Scheme for Unsteady
Problems
De Palma, P., Pascazio, G.,
Rossiello, G., Napolitano, M.
10:30 – 11:00
11:00 – 11:30
11:30 – 12:00
The Institute of Physical and Chemical
Research
Chiba University
Japan
Politecnico di Bari
Italy
Daru, V., Tenaud, C.
ENSAM
LIMSI - CNRS
France
Unsteady Simulation for Flutter
Prediction
Accurate Flow Prediction for Store
Separation from Internal Bay
Numerical Simulation of Blood Flow in
Small Vessels
Delbove, J.
Mani, M.
Khatir, Z., Sequeira, A.
AIRBUS - EGA
France
The Boeing Company
USA
Instituto Superior Técnico
Portugal
Time-accurate calculations with
approximately factored implicit
schemes
A “Parallelized Coupled NavierComputational Fluid Dynamics and
Stokes/Vortex-Panel Solver” for the
Wall Mechanics of Pre- and PostNumerical Analysis of Wind Turbines Operative Abdominal Aortic Aneurysms
Dwight, R.
Schmitz, S., Chattot, J. -J.
Scotti, C. M., Finol, E. A., Amon, C. H.
German Center for Air and Space
Travel
Germany
University of California, Davis
USA
Carnegie Mellon University
USA
Conservative Non-Linear Residual
Distribution Schemes for the
Solution of General Unsteady
Systems of Conservative Laws
Geometrical Considerations in Patient
Specific Models of a Human Aorta with
Stenosis and Aneurysm
Svensson, J., Gardhagen, R.,
Karlsson, M.
Ricciuto, M., Csik, A., Deconinck, H.
von Karman Institute for Fluid
Dynamics
Belgium
12:00 – 1:30
Himeno R., Liu, H.
Linköping University
Sweden
Lunch, Pier 4 & 5
Thursday, July 15, 2004
1:30 – 3:30
1:30 – 2:00
Session 25, Harbour A
Session 26, Harbour B
Session 27, Harbour C
Algorithms III
Fluid-Structure Interaction
Acoustics
Chair: Charles-Henri Bruneau
Chair: Nobuyuki Satofuka
Chair: Mike Giles
A New Accurate and Stable LeastSquare Method to Compute the
Gradient on Non-Orthogonal Meshes
Adaptive Solution of Steady-State
Fluid-Structure Interaction
A Hybrid FE/Spectral Analysis of
Turbofan Aeroacoustics
Etienne, S., Pelletier, D.
Duta, M. C., Giles, M. B., Laird, A.
École Polytechnique de Montréal
Canada
Oxford University
UK
Robustness of a Characteristic Finite
Element Scheme of Second Order in
Time Increment
Numerical Simulation for Impact of
Elastic Deformable Body against
Wall under Fluid Dynamic Force
Numerical Simulation of the Oscillation
in a Mixer – An Internal Aeroacoustic
Feedback System
Tabata, M.
Hashimoto, T., Morinishi, K.,
Satofuka, N.
Jorgenson, P. C. E., Loh, C. Y.
Béchaud, C., Yakobi, K.,
Archambeau, F., Mechitoua, N.
EDF R&D
France
2:00 – 2:30
Kyushu University
Japan
2:30 – 3:00
Gas-Kinetic Scheme for Hyperbolic
Viscous Flow
Kyoto Institute of Technology
Japan
NASA Glenn Research Center
USA
Fluid Structure Interaction of a
Hypersonic Generic Body-Flap
Model
Accuracy of CFD Simulations of
Acoustic Wave Phenomena in
Combustion Chambers
Mack, A., Schaefer, R., Esser, B.,
Guelhan, A.
Venkateswaran, S., Xia, G.,
Merkle, C. L.
DLR, German Aerospace Center
Germany
Purdue University
USA
A Comparison of Space-Time
Variational-Multiscale Discretizations
Two-dimensional Coupled Analysis
of Pipe Burst and Multi Components
Fluid of Very High Pressured Natural
Gas Pipeline
Computation of Gust-Cascade
Interaction using the CE/SE Method
Hulshoff, S. J.
Oda, T., Tamura, Y., Matsumoto, Y.,
Kawamura, T.
Ochanomizu University
Toyo University
University of Tokyo
Xu, K., Mao, M.
Hong Kong University of Science
and Technology, Hong Kong
China Aerodynamics Research and
Development Center, China
3:00 – 3:30
Delft University of Technology
Netherlands
Japan
3:30 – 4:00
Coffee Break, Harbour Foyer
Wang, X.-Y., Himanshu, A.,
Chang, S.-C., Jorgenson, P. C. E.
NASA Glenn Research Center
Taitech Inc.
USA
Thursday, July 15, 2004
4:00 – 5:30
4:00 – 4:30
Session 28, Harbour A
Session 29, Harbour B
Session 30, Harbour C
Upwind Schemes III
Parallel Algorithms II
High-Order Schemes III
Chair: Herman Deconinck
Chair: Gerard Degrez
Chair: Dave Darmofal
Exact Flux Linearization for
Convergence Improvement in the
Implicit Godunov Method
A Parallel Multi-Block Method for the
Unsteady Vorticity-Velocity NavierStokes Equation
Computation of Aeroacoustic Waves
with High Order Spectral Volume
Method
Men'shov, I., Nakamura, Y.
Grimaldi, A., Pascazio, G.,
Napolitano, M.
Wang, Z. J.
Nagoya University
Japan
4:30 – 5:00
Michigan State University
USA
On High-Order Fluctuation-Splitting
Schemes for Navier-Stokes
Equations
Parallelization of an Unstructured
Data Based Cell Centre Finite
Volume Code, HIFUN-3D
Discontimuous Spectral Difference
Method for Conservative Laws on
Unstructured grids
Nishikawa, H., Roe, P.
Shinde, G. S., Shende, N. V.,
Balakrishnan, N.
Liu, Y., Vinokur, M., Wang, Z.J.
University of Michigan
USA
5:00 – 5:30
Politecnico di Bari
Italy
Extension of the Roe Scheme to the
Weakly Ionised Gas for Atmospheric
Reentry
Indian Institute of Science
India
NASA Ames Research Center
Eloret Corp
USA
Parallel Turbulent Flow
Computations Using a Hybrid
Spectral/Finite-Element Method on
Beowulf Clusters
Multigrid Solution for High-Order
Discontinuous Galerkin Discretizations
of the Compressible Navier-Stokes
Equations
Vanden Abeele, D., Degrez, G.,
Snyder, D. O.
Université Libre de Bruxelles,
Belgium
Sverdrup Technology, USA
Oliver, T., Fidkowski, K.,
Darmofal, D. L.
Rouzaud, O., Soubrié, T.
ONERA
France
5:30 – 6:30
Massachusetts Institute of Technology
USA
Poster Session III, Pier 2 & 3
Upwind Schemes in DNS of
Compressible Turbulence
Finite Element Method in DomainDecomposition for Fluid-Structure
Interaction Problems
LES of Turbulent Flow around a
Simplified Railway Vehicle Model
under Cross Winds
Yanwen, M.
Moses, P., Novotny, J., Burda, P.
Nakade, K., Suzuki, M.
Chinese Academy of Sciences
China
Czech University Technology
Czech Republic
Railway Technical Research Institute
Japan
Development of Compressible
Direct Numerical Simulation of Mixed
Navier-Stokes Equations into Higher Convection in Horizontal Pipe Flow
Order DNS of Incompressible
Turbulence
Piller, M.
Nishida, H., Hatta, M.
Universita degli Studi di Trieste
Kyoto Institute of Technology
Dipartimento di Ingegneria Navale
Japan
Italy
Application of a High Resolution,
Unstructured, Solution Adaptive, Finite
Volume Method to Hypersonic Inlet
Tahir, R., Timofeev, E., Voinovich, P.,
Molder, S.
RBT Consultants, Canada
McGill University, Canada
A.F.Ioffe Physical-Technical Institute,
Russia
Ryerson Polytechnic University, Canada
Fluid Structure Interaction for Strongly
Coupled Problems Based on a
Sensitivity Analysis Technique
Vierendeels, J., Dumont, K., Dick, E.,
Verdonck, P.
Ghent University
Belgium
Numerical Simulation of Flow
Conditioners in Pipes
Large Eddy Simulation Using
Tetrahedral Elements
Von Lavante, E., Moniz-Pereira, G.,
Mickan, B.
Xu, T., Cardenas, G., Paraschivoiu, M.
University of Duisburg-Essen
Germany
Computational Fluid Dynamics
Simulation of High Temperature Raw
Materials Processing
Yang, Y., Zhou, B., Post, J. R.,
Reuter, M., A.
Delft University of Technology
The Netherlands
7:00 – 10:00
Banquet, Pier 4&5
University of Toronto
Concordia University
Canada
Friday, July 16, 2004
8:30 – 9:30
Invited Lecture, Harbour A & B
Micro Flow Simulation Using Kinetic and Continuum Approaches
Dr. Koji Morinishi
Kyoto Institute of Technology, Japan
9:30 – 10:00
10:00 – 12:00
10:00 – 10:30
Coffee Break, Harbour Foyer
Session 31, Harbour A
Session 32, Harbour B
Session 33, Harbour C
Microscale Flows
Meshless Methods
Applications IV
Chair: Koji Morinishi
Chair: Karkenahalli Srinivas
Chair: Francois Fortin
Preconditioning Method for
Compressible Near-Critical Fluids in
Micro-Channel
Parallelization of Gridfree Kinetic
Upwind Solver
Mathematical Modelling of Supersonic
Turbulent Flows in Inlets with Rotating
Cowl
Yamamoto, S.
10:30 – 11:00
Anandhanarayanan, K.,
Nagarathinam, M., Deshpande, S.M.
Tohoku University
Japan
DRDL
Indian Institute of Science
India
Comparison of Kinetic and NavierStokes Solutions for Rarefied Gas
Flows in Micro-Channels
Computation of Viscous Vortices with
Fully Meshless Method
Bedarev, I. A., Fedorova, N. N.,
Goldfeld, M. A., Falempin, F.
Institute of Theoretical and Applied
Mechanics, Russia
MBDA, France
Computational Fluid Dynamics of
Crossflow Filtration in SuspensionFeeding Fishes
Barba, L. A., Leonard, A.
Satofuka, N., Morinishi, K.,
Kamitsuji, K.
Kyoto Institute of Technology
Japan
11:00 – 11:30
11:30 – 12:00
University of Bristol, UK
California Institute of Technology,
USA
Cheer, A. Y., Cheung, S.,
Sanderson, S. L.
University of California, Davis
NASA Ames Research Center
College of William and Mary
USA
Application of the 10-Moment Model
to MEMS Flows
Gridless Computation using Unified
Coordinates
Numerical Simulation of R-m Instability
Suzuki, Y., Yamamoto, S.,
van Leer, B., Sun, Q., Boyd, I. D.
Hui, W. H., Hu, J. J.
Fu D., Ma Y., Tian B.
University of Michigan
USA
Hong Kong University of Science and
Technology
Hong Kong
Chinese Academy of Sciences
China
A Low Leakage Injection Method in
Microfluidic Chips
Viscous Flow Computations Using a
Meshless Solver, LSFD-U
Leading Edge Vortex Separation and
Efficient thrust and Efficiency of
Propulsion by Oscillating Foils
Fu, L. -M., Yang, R. -J., Lin, C. -H.,
Lee, C. -Y.
National Pingtung University of
Science and Technology
National Cheng Kung University
National Sun Yat-sen University
Taiwan
Ninewa, A., Munikrishna, N.,
Balakrishnan, N.
Indian Institute of Science
India
Young, J., Lai, J. C. S., Kaya, M.,
Tuncer, I. H.
Australian Defence Force Academy,
Australia
Middle East Technical University,
Turkey