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Keyword [High Reynolds]
Result: 1 - 20 | Page: 1 of 2
1. Numerical Research On The Hydrodynamic Characters Of A Circle Cylinder And Two Circle Cylinders In Tandem Arrangement In Uniform Cross Flow
2. The Comparison, Improvement And Application Of Turbulence Models
3. Theory And Applications Of Lattice Boltzmann Method At High Reynolds Number
4. Numerical Simulation Of Three-dimensional Flow Past Circular Cylinders At High Reynolds Numbers
5. Numerical Simulation Of Flow Around Two Prisms In Tandem Arrangement At High Reynolds Numbers
6. Experimental Study Of Generalized Logarithmic Law For High-order Moments At High Reynolds-number
7. Research On Lattice Boltzmann Simulation On High Reynolds Number Flow Around Marine Current Turbine
8. Experimental Study Of High Reynolds Number Turbulence In Atmospheric Surface Layer
9. Research On The Discrete Vortex Method Based On Instantanous Vorticity Conservation And Its Application In Vortex Induced Vibration Of Marine Risers
10. Research On Vortex Shedding And Hydrodynamic Characteristics Of A Near-plane Circular Cylinder
11. Features And Characterizations Of Large-Scale Three-Dimensional Structures In The Atmospheric Surface Layer
12. Simulation Of Cavity Flow Based On LES Method In High Reynolds Number
13. Numerical Simulation Of Vortex Induced Vibration Of A Circular Cylinder With Two DOFs Based On OpenFOAM
14. Scaling Of Wall-normal Turbulence Intensity And Vertical Eddy Structures In The Atmospheric Surface Layer
15. Influence Of The Incidental Intense Thermal Convection Events On The Atmospheric Surface Layer Wall Turbulence
16. The Variational Multiscale Methods For The Unsteady Incompressible Navier-Stokes Equations With High Reynolds Numbers
17. The Subgrid Stabilized Finite Element Methods With Backtracking Technique For The Navier-Stokes Equations At High Reynolds Numbers
18. Study On Flow Control Of Airfoil With High Reynolds Number By Synthetic Jet
19. Numerical Studey Of Tadpole Swimming In Complex Vortex Flow
20. Characterization of the influence of a favorable pressure gradient on the basic structure of a mach 5.0 high reynolds number supersonic turbulent boundary layer
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