An Open-Source Code for High-Speed Non-Equilibrium Gas–Solid Flows in OpenFOAM

This paper details the development and verification tests of an open-source code named hy2LPTFoam intended for solving high-speed non-equilibrium gas-particle flows in OpenFOAM. The solver, based on hy2Foam for high-speed non-equilibrium gas flow, integrates multiple particle force models, heat transfer models, the diffusion-based smoothing method, and the MPPIC method. The verification tests incorporate interactions between shock waves and particle curtains with varying particle volume fractions, a JPL nozzle generating a two-phase gas–particle flow, and a Mars entry body with two particle inflow mass fractions. The tests yield good physical agreement with numerical and experimental data from the literature.

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Publication Details

Journal
Aerospace
Published
2024-09-10
DOI
https://doi.org/10.3390/aerospace11090742
Citations
1
Primary Topic
Fluid Dynamics and Heat Transfer
Type
article
Field-Weighted Citation Impact
0.37

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article

An Open-Source Code for High-Speed Non-Equilibrium Gas–Solid Flows in OpenFOAM

Ziqu Cao, Yong Zhang, Xiaofeng Zhang
1 citations
Aerospace
Fluid Dynamics and Heat Transfer
0.37
article

An Open-Source Code for High-Speed Non-Equilibrium Gas–Solid Flows in OpenFOAM

Ziqu Cao, Yong Zhang, Xiaofeng Zhang
article en
1 citations

Abstract

This paper details the development and verification tests of an open-source code named hy2LPTFoam intended for solving high-speed non-equilibrium gas-particle flows in OpenFOAM. The solver, based on hy2Foam for high-speed non-equilibrium gas flow, integrates multiple particle force models, heat transfer models, the diffusion-based smoothing method, and the MPPIC method. The verification tests incorporate interactions between shock waves and particle curtains with varying particle volume fractions, a JPL nozzle generating a two-phase gas–particle flow, and a Mars entry body with two particle inflow mass fractions. The tests yield good physical agreement with numerical and experimental data from the literature.

AerospaceVol. 11(9)
Shanghai Micro Satellite Engineering Center (CN), Innovation Academy for Microsatellites of Chinese Academy of Sciences
Chinese Academy of Sciences
Openalex Percentile: Top 44%
Fluid Dynamics and Heat Transfer
0.37
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