Development of parallel direct simulation Monte Carlo method using a cut-cell Cartesian grid on a single graphics processor

DOI10.1016/J.COMPFLUID.2014.06.003zbMath1391.76680OpenAlexW2074093112MaRDI QIDQ1641519

Y. Aharonov

Publication date: 19 June 2018

Published in: Computers and Fluids (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/j.compfluid.2014.06.003

zbMATH Keywords

variable time-stepcut-celltransient adaptive sub-cell

Mathematics Subject Classification ID

Monte Carlo methods (65C05) Rarefied gas flows, Boltzmann equation in fluid mechanics (76P05) Particle methods and lattice-gas methods (76M28) Hypersonic flows (76K05)

Related Items (3)

DSMC simulation of hypersonic flows using an improved SBT-TAS technique ⋮ A new cut-cell algorithm for DSMC simulations of rarefied gas flows around immersed moving objects ⋮ Evaluation of the generalized Bernoulli trial-transient adaptive subcell (GBT-TAS) collision scheme in treating rarefied gas flows

Uses Software

• CUDA
• MONACO

Cites Work

• Unnamed Item
• Implementation of a transient adaptive sub-cell module for the parallel-DSMC code using unstructured grids
• Parallel three-dimensional DSMC method using mesh refinement and variable time-step scheme
• Vectorization of a Monte Carlo simulation scheme for nonequilibrium gas dynamics
• A convergence proof for Bird's direct simulation Monte Carlo method for the Boltzmann equation
• Parallel three-dimensional direct simulation Monte Carlo method and its applications.
• Scalar and parallel optimized implementation of the direct simulation Monte Carlo method
• A parallel implementation of the direct simulation Monte Carlo method
• Strategies for efficient particle resolution in the direct simulation Monte Carlo method.
• Robust cut-cell algorithms for DSMC implementations employing multi-level Cartesian grids
• Effects of continuum breakdown on hypersonic aerothermodynamics
• Experiments on shock wave reflection transition and hysteresis in low-noise wind tunnel

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