A new high resolution scheme for compressible viscous flows with shocks

S. Tatsumi; Luigi Martinelli; A. Jameson

A new high resolution scheme for compressible viscous flows with shocks

S. Tatsumi, Luigi Martinelli, A. Jameson

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

Abstract

A new flux splitting and limiting technique which yields one-point stationary shock capturing is presented. The technique is applied to the full Navier Stokes and Reynolds Averaged Navier-Stokes equations. Calculations of laminar boundary layers at subsonic and supersonic speeds are presented together with calculations of transonic flows around airfoils. The results exhibit very good agreement with theoretical solutions and existing experimental data. It is found that the proposed scheme improves the resolution of viscous flows while maintaining excellent one-point shock capturing characteristics.

Original language	English (US)
Pages	1-15
Number of pages	15
State	Published - 1995
Event	33rd Aerospace Sciences Meeting and Exhibit, 1995 - Reno, United States Duration: Jan 9 1995 → Jan 12 1995

Other

Other	33rd Aerospace Sciences Meeting and Exhibit, 1995
Country/Territory	United States
City	Reno
Period	1/9/95 → 1/12/95

All Science Journal Classification (ASJC) codes

Space and Planetary Science
Aerospace Engineering

Cite this

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title = "A new high resolution scheme for compressible viscous flows with shocks",

abstract = "A new flux splitting and limiting technique which yields one-point stationary shock capturing is presented. The technique is applied to the full Navier Stokes and Reynolds Averaged Navier-Stokes equations. Calculations of laminar boundary layers at subsonic and supersonic speeds are presented together with calculations of transonic flows around airfoils. The results exhibit very good agreement with theoretical solutions and existing experimental data. It is found that the proposed scheme improves the resolution of viscous flows while maintaining excellent one-point shock capturing characteristics.",

author = "S. Tatsumi and Luigi Martinelli and A. Jameson",

note = "Publisher Copyright: {\textcopyright} 1995, by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.; 33rd Aerospace Sciences Meeting and Exhibit, 1995 ; Conference date: 09-01-1995 Through 12-01-1995",

year = "1995",

language = "English (US)",

pages = "1--15",

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TY - CONF

T1 - A new high resolution scheme for compressible viscous flows with shocks

AU - Tatsumi, S.

AU - Martinelli, Luigi

AU - Jameson, A.

PY - 1995

Y1 - 1995

N2 - A new flux splitting and limiting technique which yields one-point stationary shock capturing is presented. The technique is applied to the full Navier Stokes and Reynolds Averaged Navier-Stokes equations. Calculations of laminar boundary layers at subsonic and supersonic speeds are presented together with calculations of transonic flows around airfoils. The results exhibit very good agreement with theoretical solutions and existing experimental data. It is found that the proposed scheme improves the resolution of viscous flows while maintaining excellent one-point shock capturing characteristics.

AB - A new flux splitting and limiting technique which yields one-point stationary shock capturing is presented. The technique is applied to the full Navier Stokes and Reynolds Averaged Navier-Stokes equations. Calculations of laminar boundary layers at subsonic and supersonic speeds are presented together with calculations of transonic flows around airfoils. The results exhibit very good agreement with theoretical solutions and existing experimental data. It is found that the proposed scheme improves the resolution of viscous flows while maintaining excellent one-point shock capturing characteristics.

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M3 - Paper

AN - SCOPUS:84963610742

SP - 1

EP - 15

T2 - 33rd Aerospace Sciences Meeting and Exhibit, 1995

Y2 - 9 January 1995 through 12 January 1995

ER -

A new high resolution scheme for compressible viscous flows with shocks

Abstract

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All Science Journal Classification (ASJC) codes

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