
pmid: 16214688
A low Mach number approximation (LMNA) of the Navier-Stokes equations is widely used in numerical methods for the simulation of low-speed thermal and athermal flows. The advanced lattice Boltzmann approach (Bhatnagar-Gross-Krook) for the solution of the LMNA equations is discussed and its performance is compared with the performance of the commercial CFD code FLUENT 5.
low Mach number approximation, Models, Statistical, multiscale lattice Boltzmann method, Models, Biological, Navier Stokes equations, Diffusion, Kinetics, Models, Chemical, Particle methods and lattice-gas methods, Quantum Theory, Computer Simulation, grid refinement, Colloids, Gases, Particle Size, General aerodynamics and subsonic flows, CFD code FLUENT 5, Rheology
low Mach number approximation, Models, Statistical, multiscale lattice Boltzmann method, Models, Biological, Navier Stokes equations, Diffusion, Kinetics, Models, Chemical, Particle methods and lattice-gas methods, Quantum Theory, Computer Simulation, grid refinement, Colloids, Gases, Particle Size, General aerodynamics and subsonic flows, CFD code FLUENT 5, Rheology
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