2015
DOI: 10.1016/j.paerosci.2014.12.002
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Rarefied gas flow simulations using high-order gas-kinetic unified algorithms for Boltzmann model equations

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Cited by 76 publications
(42 citation statements)
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“…Such waves are generally associated with the boundary layer and appear only in the case of large gradients in the flow variables (e.g., velocity, density, temperature). It should be added that the thickness of the shock layer is greater at higher altitudes (e.g., for illustrative examples see Li et al, 2015). Moreover, the shock layers may be optically thin, characterized by the absence of re-absorption of radiation emitted from other parts of the gas.…”
Section: Figurementioning
confidence: 99%
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“…Such waves are generally associated with the boundary layer and appear only in the case of large gradients in the flow variables (e.g., velocity, density, temperature). It should be added that the thickness of the shock layer is greater at higher altitudes (e.g., for illustrative examples see Li et al, 2015). Moreover, the shock layers may be optically thin, characterized by the absence of re-absorption of radiation emitted from other parts of the gas.…”
Section: Figurementioning
confidence: 99%
“…A comprehensive discussion on numerical modeling of hypersonic flow is well beyond the scope of this paper, considering that this topic is extensive, well researched, and well represented in literature (e.g., see Sarma, 2000;Bertin et al, 2003;Longo et al, 2007;Gnoffo et al, 2010;McNamara et al, 2011;Boyd, 2014;Li et al, 2015;and references therein). Nevertheless, in this section we present a brief outline of numerical approaches relevant to meteors.…”
Section: Numerical Approachmentioning
confidence: 99%
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“…However, even with the advanced numerical algorithms and simplified kinetic models, direct simulations of practical 3D problems by DVM are still computationally expensive regarding both the floating point operations and the memory requirement, due to the sheer number of grid points in the phase space (physical space and molecular velocity space). In most practical simulations especially involving high speed flows, massively parallel supercomputing facilities are indispensable [31,22,[32][33][34][35][36][37]. Various techniques have been proposed to reduce the grid points, e.g., the adaptive local refinement for the spatial and velocity grids [38][39][40][41][42].…”
Section: Introductionmentioning
confidence: 99%
“…In recent years, a variety of kinetic models based on Boltzmann equation are proposed to simulate non-equilibrium flows [4][5][6][7][8][9][10][11][12][13][14][15][16][17][18][19][20][21][22][23]. The Discrete Boltzmann Method (DBM) [24][25][26][27][28][29][30][31][32][33][34][35][36][37] recently developed from the Lattice Boltzmann Method (LBM) [38][39][40][41][42][43][44][45][46][47][48][49][50][51][52] belongs to this category.…”
Section: Introductionmentioning
confidence: 99%