Satellite design verification study based on thruster plume flow impingement effects using parallel DSMC method

DOI10.1016/J.COMPFLUID.2018.03.034zbMath1410.76329OpenAlexW2793358833WikidataQ130183523 ScholiaQ130183523MaRDI QIDQ1615468

Kyun Ho Lee

Publication date: 31 October 2018

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

Full work available at URL: https://doi.org/10.1016/j.compfluid.2018.03.034

zbMATH Keywords

thrusterdirect simulation Monte Carlo (DSMC)plume gas flowsatellite design

Mathematics Subject Classification ID

Monte Carlo methods (65C05) Parallel numerical computation (65Y05) Software, source code, etc. for problems pertaining to fluid mechanics (76-04)

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