A novel algorithm for implementing a specified wall heat flux in DSMC: application to micro/nano flows and hypersonic flows
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Publication:1646811
DOI10.1016/j.compfluid.2015.12.008zbMath1390.76799OpenAlexW2200950927MaRDI QIDQ1646811
Publication date: 26 June 2018
Published in: Computers and Fluids (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1016/j.compfluid.2015.12.008
rarefactionDSMCcontrolling factorhybrid MIT-ITSmodified iterative technique (MIT)specified wall heat flux
Related Items (2)
Conserved method for specified heat flux boundary in UGKS simulation of microscale gas flow ⋮ Investigating the Simulation Rate of an Axially Symmetric Rarefied Gas Flow Using v-DSMC
Cites Work
- Unnamed Item
- Study on micronozzle flow and propulsion performance using DSMC and continuum methods
- Analytical solution of plane Couette flow in the transition regime and comparison with direct simulation Monte Carlo data
- Global existence of solutions for a model Boltzmann equation
- Analytical solution of gaseous slip flow in long microchannels
- DSMC simulation of hypersonic flows using an improved SBT-TAS technique
- Atomistic simulation of rarefied gas natural convection in a finite enclosure using a novel wall-fluid molecular collision rule for adiabatic solid walls
- Microflows and nanoflows. Fundamentals and simulation. Foreword by Chih-Ming Ho.
- Mass flow rate prediction of pressure-temperature-driven gas flows through micro/nanoscale channels
- On DSMC Calculations of Rarefied Gas Flows with Small Number of Particles in Cells
- Direct simulation of gas flows at the molecular level
- Investigation of rarefied supersonic flows into rectangular nanochannels using a three-dimensional direct simulation Monte Carlo method
- Heat-flux-specified boundary treatment for gas flow and heat transfer in microchannel using direct simulation Monte Carlo method
- A generalized hard-sphere model for Monte Carlo simulation
- Extending the Navier–Stokes solutions to transition regime in two-dimensional micro- and nanochannel flows using information preservation scheme
- Numerical Simulation of Rarefied Gas Flows with Specified Heat Flux Boundary Conditions
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