Gas-kinetic BGK scheme for hypersonic viscous flow

Mei-Liang Mao; Kun Xu

doi:10.1007/3-540-31801-1_23

Gas-kinetic BGK scheme for hypersonic viscous flow

Mei-Liang Mao, Kun Xu

The Hong Kong University of Science and Technology

Research output: Contribution to conference › Conference Paper › peer-review

Abstract

This paper is about the application of a gas-kinetic scheme based on the Bhatnagar-Gross-Krook (BGK) model for the Navier-Stokes equations in the study of hypersonic viscous flow. In the laminar hypersonic viscous flow computations, complicated flow phenomena, i.e., shock boundary layer interaction, flow separation, and viscous/inviscid interaction, will be encountered. The cases studied include the type IV shock-shock interaction around a circular cylinder and hypersonic flow passing through a double-cone geometry.

Original language	English
DOIs	https://doi.org/10.1007/3-540-31801-1_23
Publication status	Published - 2004
Event	Computational Fluid Dynamics 2004, Proceedings - Duration: 1 Jan 2004 → 1 Jan 2004

Conference

Conference	Computational Fluid Dynamics 2004, Proceedings
Period	1/01/04 → 1/01/04

ISBNs

['3-540-31800-3']

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10.1007/3-540-31801-1_23

Cite this

@conference{c58c369634904fb39cfb5a0ebf49e49b,

title = "Gas-kinetic BGK scheme for hypersonic viscous flow",

abstract = "This paper is about the application of a gas-kinetic scheme based on the Bhatnagar-Gross-Krook (BGK) model for the Navier-Stokes equations in the study of hypersonic viscous flow. In the laminar hypersonic viscous flow computations, complicated flow phenomena, i.e., shock boundary layer interaction, flow separation, and viscous/inviscid interaction, will be encountered. The cases studied include the type IV shock-shock interaction around a circular cylinder and hypersonic flow passing through a double-cone geometry.",

author = "Mei-Liang Mao and Kun Xu",

year = "2004",

doi = "10.1007/3-540-31801-1\_23",

language = "English",

note = "Computational Fluid Dynamics 2004, Proceedings ; Conference date: 01-01-2004 Through 01-01-2004",

}

TY - CONF

T1 - Gas-kinetic BGK scheme for hypersonic viscous flow

AU - Mao, Mei-Liang

AU - Xu, Kun

PY - 2004

Y1 - 2004

N2 - This paper is about the application of a gas-kinetic scheme based on the Bhatnagar-Gross-Krook (BGK) model for the Navier-Stokes equations in the study of hypersonic viscous flow. In the laminar hypersonic viscous flow computations, complicated flow phenomena, i.e., shock boundary layer interaction, flow separation, and viscous/inviscid interaction, will be encountered. The cases studied include the type IV shock-shock interaction around a circular cylinder and hypersonic flow passing through a double-cone geometry.

AB - This paper is about the application of a gas-kinetic scheme based on the Bhatnagar-Gross-Krook (BGK) model for the Navier-Stokes equations in the study of hypersonic viscous flow. In the laminar hypersonic viscous flow computations, complicated flow phenomena, i.e., shock boundary layer interaction, flow separation, and viscous/inviscid interaction, will be encountered. The cases studied include the type IV shock-shock interaction around a circular cylinder and hypersonic flow passing through a double-cone geometry.

UR - https://www.webofscience.com/wos/woscc/full-record/WOS:000240583500023

UR - https://openalex.org/W24765676

U2 - 10.1007/3-540-31801-1_23

DO - 10.1007/3-540-31801-1_23

M3 - Conference Paper

T2 - Computational Fluid Dynamics 2004, Proceedings

Y2 - 1 January 2004 through 1 January 2004

ER -

Gas-kinetic BGK scheme for hypersonic viscous flow

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