Study on micronozzle flow and propulsion performance using DSMC and continuum methods
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Publication:612320
DOI10.1007/s10409-006-0020-yzbMath1202.76110OpenAlexW2083020598MaRDI QIDQ612320
Genxuan Zhang, Yi Liang Chen, Xianfeng Zhang, Ming-hou Liu
Publication date: 28 December 2010
Published in: Acta Mechanica Sinica (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1007/s10409-006-0020-y
Navier-Stokes equations for incompressible viscous fluids (76D05) Rarefied gas flows, Boltzmann equation in fluid mechanics (76P05)
Related Items (4)
A novel algorithm for implementing a specified wall heat flux in DSMC: application to micro/nano flows and hypersonic flows ⋮ Hybrid simulations of rarefied supersonic gas flows in micro-nozzles ⋮ Information preservation optimization method based on the advection upstream splitting method in supersonic rarefied flow simulation ⋮ A computational study of gas flow in a De-Laval micronozzle at different throat diameters
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