Vectorization of a Monte Carlo simulation scheme for nonequilibrium gas dynamics

DOI10.1016/0021-9991(91)90243-EzbMath0726.76076OpenAlexW2021653640MaRDI QIDQ802981

Iain D. Boyd

Publication date: 1991

Published in: Journal of Computational Physics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/0021-9991(91)90243-e

zbMATH Keywords

hypersonic flowMonte Carlo schemenon-equilibrium gas dynamicsnumerical performanceexpanding gas through an axisymmetric nozzleone-dimensional standing shock wave

Mathematics Subject Classification ID

Shock waves and blast waves in fluid mechanics (76L05) Transonic flows (76H05) Gas dynamics (general theory) (76N15)

Related Items (6)

Development of parallel direct simulation Monte Carlo method using a cut-cell Cartesian grid on a single graphics processor ⋮ Deterministic solution of the spatially homogeneous Boltzmann equation using discontinuous Galerkin discretizations in the velocity space ⋮ A deterministic-stochastic method for computing the Boltzmann collision integral in \(\mathcal{O}(MN)\) operations ⋮ A parallel implementation of the direct simulation Monte Carlo method ⋮ PID feedback for load-balanced parallel gridless DSMC ⋮ Application highlights of the DSMC analysis code (DAC) software for simulating rarefied flows

Cites Work

• Unnamed Item
• On the use of the modified Nanbu direct simulation scheme
• Rarefied gas flow analysis by direct simulation Monte Carlo method in body-fitted coordinate system
• On simulation methods for solving the Boltzmann equation

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