Benchmark numerical simulations of rarefied non-reacting gas flows using an open-source DSMC code

被引:43
|
作者
Palharini, Rodrigo C. [1 ]
White, Craig [2 ]
Scanlon, Thomas J. [3 ,4 ]
Brown, Richard E. [3 ]
Borg, Matthew K. [5 ,6 ]
Reese, Jason M. [5 ]
机构
[1] Inst Aeronaut & Espaco, Div Aerodinam, BR-12228904 Sao Jose Dos Campos, SP, Brazil
[2] Univ Glasgow, Sch Engn, Glasgow G12 8QQ, Lanark, Scotland
[3] Univ Strathclyde, Dept Mech & Aerosp Engn, Glasgow G1 1XJ, Lanark, Scotland
[4] Univ Strathclyde, James Weir Fluids Lab, Glasgow, Lanark, Scotland
[5] Univ Edinburgh, Sch Engn, Edinburgh EH9 3JL, Midlothian, Scotland
[6] Univ Strathclyde, Ctr Future Air Space Transportat Technol, Glasgow, Lanark, Scotland
基金
英国工程与自然科学研究理事会;
关键词
DSMC; Benchmark; Open-source; Rarefied gas dynamics; Aerodynamics; Low/high speed flows; MONTE-CARLO-SIMULATION; HYPERSONIC CONDITIONS; HEAT-TRANSFER; PARTICLE SIMULATIONS; LEADING-EDGE; VALIDATION; MODEL; EQUATIONS; NUMBER; VERIFICATION;
D O I
10.1016/j.compfluid.2015.07.021
中图分类号
TP39 [计算机的应用];
学科分类号
081203 ; 0835 ;
摘要
Validation and verification represent an important element in the development of a computational code. The aim is establish both confidence in the algorithm and its suitability for the intended purpose. In this paper, a direct simulation Monte Carlo solver, called dsmcFoam, is carefully investigated for its ability to solve low and high speed non-reacting gas flows in simple and complex geometries. The test cases are: flow over sharp and truncated flat plates, the Mars Pathfinder probe, a micro-channel with heated internal steps, and a simple micro-channel. For all the cases investigated, dsmcFoam demonstrates very good agreement with experimental and numerical data available in the literature. (C) 2015 Elsevier Ltd. All rights reserved.
引用
收藏
页码:140 / 157
页数:18
相关论文
共 13 条
  • [1] An open source, parallel DSMC code for rarefied gas flows in arbitrary geometries
    Scanlon, T. J.
    Roohi, E.
    White, C.
    Darbandi, M.
    Reese, J. M.
    [J]. COMPUTERS & FLUIDS, 2010, 39 (10) : 2078 - 2089
  • [2] Hypersonic Simulations using Open-Source CFD and DSMC Solvers
    Casseau, V.
    Scanlon, T. J.
    John, B.
    Emerson, D. R.
    Brown, R. E.
    [J]. 30TH INTERNATIONAL SYMPOSIUM ON RAREFIED GAS DYNAMICS (RGD 30), 2016, 1786
  • [3] Numerical Simulation of Non-Reacting and Reacting Flows in a 5MW Commercial Gas Turbine Combustor
    Jeong, Daero
    Huh, Kang Y.
    [J]. PROCEEDINGS OF THE ASME TURBO EXPO 2009, VOL 2, 2009, : 739 - 748
  • [4] THE SIMULATIONS OF FLOW AND HEAT OVER MICROSCALE SENSORS IN SUPERSONIC RAREFIED GAS FLOWS USING DSMC
    Darbandi, Masoud
    Mosayebi, Ghasem
    [J]. PROCEEDINGS OF THE ASME 5TH INTERNATIONAL CONFERENCE ON MICRO/NANOSCALE HEAT AND MASS TRANSFER, 2016, VOL 2, 2016,
  • [5] VALIDATION OF OPEN-SOURCE SPH CODE DUALSPHYSICS FOR NUMERICAL SIMULATIONS OF WATER ENTRY AND EXIT OF A RIGID BODY
    Buruchenko, Sergei K.
    Canelas, Ricardo B.
    [J]. PROCEEDINGS OF THE ASME 36TH INTERNATIONAL CONFERENCE ON OCEAN, OFFSHORE AND ARCTIC ENGINEERING, 2017, VOL 2, 2017,
  • [6] A new open-source software developed for numerical simulations using discrete modeling methods
    Kozicki, J.
    Donze, F. V.
    [J]. COMPUTER METHODS IN APPLIED MECHANICS AND ENGINEERING, 2008, 197 (49-50) : 4429 - 4443
  • [7] Numerical Simulations of the Flow Dynamics in a Tube with Inclined Fins Using Open-Source Software
    Real-Ramirez, Cesar Augusto
    Carvajal-Mariscal, Ignacio
    Gonzalez-Trejo, Jesus
    Gabbasov, Ruslan
    Miranda-Tello, Jose Raul
    Klapp, Jaime
    [J]. FLUIDS, 2022, 7 (08)
  • [8] Benchmark simulations of flow past rigid bodies using an open-source, sharp interface immersed boundary method
    Senturk, Utku
    Brunner, Daniel
    Jasak, Hrvoje
    Herzog, Nicoleta
    Rowley, Clarence W.
    Smits, Alexander J.
    [J]. Progress in Computational Fluid Dynamics, 2019, 19 (04): : 205 - 219
  • [9] Benchmark simulations of flow past rigid bodies using an open-source, sharp interface immersed boundary method
    Senturk, Utku
    Brunner, Daniel
    Jasak, Hrvoje
    Herzog, Nicoleta
    Rowley, Clarence W.
    Smits, Alexander J.
    [J]. PROGRESS IN COMPUTATIONAL FLUID DYNAMICS, 2019, 19 (04): : 205 - 219
  • [10] Numerical Simulations of Unsteady Flows From Rarefied Transition to Continuum Using Gas-Kinetic Unified Algorithm
    Wu, Junlin
    Li, Zhihui
    Peng, Aoping
    Jiang, Xinyu
    [J]. ADVANCES IN APPLIED MATHEMATICS AND MECHANICS, 2015, 7 (05) : 569 - 596