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An accurate curved boundary treatment in the lattice boltzmann method
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Luo, Li-Shi Mei, Renwei Shyy, We |
| Organization | The National Aeronautics and Space Administration (NASA) |
| Copyright Year | 2000 |
| Abstract | The lattice Boltzmann equation (LBE) is an alternative kinetic method capable of solving hydrodynamics for various systems. Major advantages of the method are owing to the fact that the solution for the particle distribution functions is explicit, easy to implement, and natural to parallelize. Because the method often uses uniform regular Cartesian lattices in space, curved boundaries axe often approximated by a series of stairs that leads to reduction in computational accuracy. In this work, a second-order accurate treatment of boundary condition in the LBE method is developed for a curved boundary. The proposed treatment of the curved boundaries is ail improvement of a scheme due to Filippova and Hanel. The proposed treatment for curved boundaries is tested against several flow problems: 2-D channel flows with constant and oscillating pressure gradients for which analytic solutions are known, flow due to ail impulsively started wall, lid-driven square cavity flow, and uniform flow over a column of circular cylinders. The second-order accuracy is observed with solid boundary arbitrarily placed between lattice nodes. The proposed boundary condition has well behaved stability characteristics when the relaxation time is close to 1/2, the zero limit of viscosity. The improvement call make a substantial contribution toward simulating practical fluid flow problems using the lattice Boltzmann method. |
| File Size | 1274547 |
| File Format | |
| Alternate Webpage(s) | http://www.archive.org/details/nasa_techdoc_20000029581 |
| Archival Resource Key | ark:/13960/t93787p2g |
| Language | English |
| Publisher Date | 2000-02-01 |
| Publisher Institution | Langley Research Center |
| Access Restriction | Open |
| Subject Keyword | Launch Windows Planar Structures Orbital Maneuvers Spacecraft Performance Low Earth Orbits Mars Missions Elliptical Orbits Spacecraft Launching Hyperbolic Trajectories Time Dependence Oblate Spheroids Energy Levels Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
