2019
DOI: 10.1016/j.jcp.2019.05.031
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Hybrid recursive regularized thermal lattice Boltzmann model for high subsonic compressible flows

Abstract: A thermal lattice Boltzmann model with a hybrid recursive regularization (HRR) collision operator is developed on standard lattices for simulation of subsonic and sonic compressible flows without shock. The approach is hybrid: mass and momentum conservation equations are solved using a lattice Boltzmann solver, while the energy conservation is solved under entropy form with a finite volume solver. The defect of Galilean invariance related to Mach number is corrected by the third order equilibrium distribution … Show more

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Cited by 110 publications
(155 citation statements)
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“…Considering that the third-order equilibrium distribution function and recursive regularized collision model exhibit considerably better performance on numerical stability and accuracy compared to the original LBGK model [17,[45][46][47][48][49], a recursive regularized collision model associated with the third-order equilibrium distribution function is employed as the collision model. The lattice Boltzmann equation Eq.…”
Section: The Recursive Regularized Lattice-boltzmann Solvermentioning
confidence: 99%
“…Considering that the third-order equilibrium distribution function and recursive regularized collision model exhibit considerably better performance on numerical stability and accuracy compared to the original LBGK model [17,[45][46][47][48][49], a recursive regularized collision model associated with the third-order equilibrium distribution function is employed as the collision model. The lattice Boltzmann equation Eq.…”
Section: The Recursive Regularized Lattice-boltzmann Solvermentioning
confidence: 99%
“…However, apart from increased computational cost, a limited temperature range is another restriction of high-order lattices [16]. Several models have also been proposed in the literature based on standard lattices [17][18][19][20][21] for simulation of compressible flows; however, to the best of our knowledge, none of them were so far successful in simulating supersonic flows involving shock waves.…”
Section: Introductionmentioning
confidence: 99%
“…The first-order nonequilibrium contributions f (1) α can be computed via projection onto the Hermite polynomial basis and/or the CE expansion [8,39]. The latter approach, more commonly referred to as recursive regularized (RR) LBM, leads to pronounced stability improvements for high-Reynolds-number flows in both weakly and fully compressible regimes [9,14,[39][40][41][42][43].…”
Section: Introductionmentioning
confidence: 99%