Evaluation of the SBT-TAS collision scheme on treating unsteady flows
DOI10.1016/j.euromechflu.2016.12.002zbMath1408.76455OpenAlexW2566381648MaRDI QIDQ1672151
Ehsan Roohi, Seyyed Moein Madani
Publication date: 7 September 2018
Published in: European Journal of Mechanics. B. Fluids (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1016/j.euromechflu.2016.12.002
vortex sheddingunsteady flowdirect simulation Monte Carlo (DSMC)nearest neighbor (NN)simplified Bernoulli trials on transient adaptive subcells (SBT-TAS)
Monte Carlo methods (65C05) Stochastic analysis applied to problems in fluid mechanics (76M35) Rarefied gas flows, Boltzmann equation in fluid mechanics (76P05)
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Cites Work
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- Implementation of a transient adaptive sub-cell module for the parallel-DSMC code using unstructured grids
- Implementation of unsteady sampling procedures for the parallel direct simulation Monte Carlo method
- A convergence proof for Bird's direct simulation Monte Carlo method for the Boltzmann equation
- Investigation of aerodynamic characteristics of rarefied flow around NACA 0012 airfoil using DSMC and NS solvers
- DSMC simulation of hypersonic flows using an improved SBT-TAS technique
- Particle Monte Carlo Algorithms with Small Number of Particles in Grid Cells
- On DSMC Calculations of Rarefied Gas Flows with Small Number of Particles in Cells
- Parallel DSMC method using dynamic domain decomposition
- Direct simulation of gas flows at the molecular level
- Monte Carlo analysis of macroscopic fluctuations in a rarefied hypersonic flow around a cylinder
- Rayleigh–Bénard flow of a rarefied gas and its attractors. I. Convection regime
- On a simulation scheme for the Boltzmann equation
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