A computational technique for high enthalpy shock tube and shock tunnel flow simulation

Y. Sheng; J. P. Sislian; J. J. Liu

doi:10.1007/s001930050114

A computational technique for high enthalpy shock tube and shock tunnel flow simulation

Y. Sheng, J. P. Sislian, J. J. Liu

Department of Engineering Science

Research output: Contribution to journal › Article › peer-review

6 Citations (Scopus)

Abstract

A contact discontinuity tracking method with a specially designed moving grid is developed to eliminate the interface smearing completely. In order to precisely locate the contact surface, an updated Riemann solver for unsteady one-dimensional inviscid flows is also developed to allow consideration of the specific heat ratio change across the shock wave. These two new computational techniques are illustrated in a high Mach number shock tube flow field computation.

Original language	English
Pages (from-to)	203-214
Number of pages	12
Journal	Shock Waves
Volume	8
Issue number	4
DOIs	https://doi.org/10.1007/s001930050114
Publication status	Published - 1998

All Science Journal Classification (ASJC) codes

Mechanical Engineering
General Physics and Astronomy

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10.1007/s001930050114

Cite this

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title = "A computational technique for high enthalpy shock tube and shock tunnel flow simulation",

abstract = "A contact discontinuity tracking method with a specially designed moving grid is developed to eliminate the interface smearing completely. In order to precisely locate the contact surface, an updated Riemann solver for unsteady one-dimensional inviscid flows is also developed to allow consideration of the specific heat ratio change across the shock wave. These two new computational techniques are illustrated in a high Mach number shock tube flow field computation.",

author = "Y. Sheng and Sislian, {J. P.} and Liu, {J. J.}",

year = "1998",

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journal = "Shock Waves",

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AU - Sislian, J. P.

AU - Liu, J. J.

PY - 1998

Y1 - 1998

N2 - A contact discontinuity tracking method with a specially designed moving grid is developed to eliminate the interface smearing completely. In order to precisely locate the contact surface, an updated Riemann solver for unsteady one-dimensional inviscid flows is also developed to allow consideration of the specific heat ratio change across the shock wave. These two new computational techniques are illustrated in a high Mach number shock tube flow field computation.

AB - A contact discontinuity tracking method with a specially designed moving grid is developed to eliminate the interface smearing completely. In order to precisely locate the contact surface, an updated Riemann solver for unsteady one-dimensional inviscid flows is also developed to allow consideration of the specific heat ratio change across the shock wave. These two new computational techniques are illustrated in a high Mach number shock tube flow field computation.

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JO - Shock Waves

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ER -

A computational technique for high enthalpy shock tube and shock tunnel flow simulation

Abstract

All Science Journal Classification (ASJC) codes

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