NUMERICAL SIMULATION OF SEVERAL SHOCK-SEPARATED BOUNDARY-LAYER INTERACTION FLOWS USING ZERO- AND TWO-EQUATION TURBULENCE MODELS.

Galen R. Peters; Ramesh K. Agarwal; Jerry E. Deese

NUMERICAL SIMULATION OF SEVERAL SHOCK-SEPARATED BOUNDARY-LAYER INTERACTION FLOWS USING ZERO- AND TWO-EQUATION TURBULENCE MODELS.

Galen R. Peters, Ramesh K. Agarwal, Jerry E. Deese

Research output: Contribution to journal › Conference article › peer-review

Abstract

Two-dimensional shock/boundary-layer interaction flows are studied numerically by solving the mass-averaged, compressible, thin-layer Navier-Stokes equations in conjunction with a zero-equation Baldwin-Lomax and a two-equation Jones-Launder (low-Reynolds-number form of k- epsilon ) turbulence model. The subsonic turbulent boundary layer over a flat plate, the normal and oblique impingement of a shock wave on a turbulent flat-plate boundary-layer, the shock/turbulent-boundary-layer interaction in a compression corner, and the transonic viscous flowfield around an airfoil are calculated. Numerical results are compared with the calculations of other investigators and with experimental data.

Original language	English
Journal	AIAA Paper
State	Published - 1986

Cite this

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title = "NUMERICAL SIMULATION OF SEVERAL SHOCK-SEPARATED BOUNDARY-LAYER INTERACTION FLOWS USING ZERO- AND TWO-EQUATION TURBULENCE MODELS.",

abstract = "Two-dimensional shock/boundary-layer interaction flows are studied numerically by solving the mass-averaged, compressible, thin-layer Navier-Stokes equations in conjunction with a zero-equation Baldwin-Lomax and a two-equation Jones-Launder (low-Reynolds-number form of k- epsilon ) turbulence model. The subsonic turbulent boundary layer over a flat plate, the normal and oblique impingement of a shock wave on a turbulent flat-plate boundary-layer, the shock/turbulent-boundary-layer interaction in a compression corner, and the transonic viscous flowfield around an airfoil are calculated. Numerical results are compared with the calculations of other investigators and with experimental data.",

author = "Peters, {Galen R.} and Agarwal, {Ramesh K.} and Deese, {Jerry E.}",

year = "1986",

language = "English",

journal = "AIAA Paper",

issn = "0146-3705",

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T1 - NUMERICAL SIMULATION OF SEVERAL SHOCK-SEPARATED BOUNDARY-LAYER INTERACTION FLOWS USING ZERO- AND TWO-EQUATION TURBULENCE MODELS.

AU - Peters, Galen R.

AU - Agarwal, Ramesh K.

AU - Deese, Jerry E.

PY - 1986

Y1 - 1986

N2 - Two-dimensional shock/boundary-layer interaction flows are studied numerically by solving the mass-averaged, compressible, thin-layer Navier-Stokes equations in conjunction with a zero-equation Baldwin-Lomax and a two-equation Jones-Launder (low-Reynolds-number form of k- epsilon ) turbulence model. The subsonic turbulent boundary layer over a flat plate, the normal and oblique impingement of a shock wave on a turbulent flat-plate boundary-layer, the shock/turbulent-boundary-layer interaction in a compression corner, and the transonic viscous flowfield around an airfoil are calculated. Numerical results are compared with the calculations of other investigators and with experimental data.

AB - Two-dimensional shock/boundary-layer interaction flows are studied numerically by solving the mass-averaged, compressible, thin-layer Navier-Stokes equations in conjunction with a zero-equation Baldwin-Lomax and a two-equation Jones-Launder (low-Reynolds-number form of k- epsilon ) turbulence model. The subsonic turbulent boundary layer over a flat plate, the normal and oblique impingement of a shock wave on a turbulent flat-plate boundary-layer, the shock/turbulent-boundary-layer interaction in a compression corner, and the transonic viscous flowfield around an airfoil are calculated. Numerical results are compared with the calculations of other investigators and with experimental data.

UR - http://www.scopus.com/inward/record.url?scp=0022581676&partnerID=8YFLogxK

M3 - Conference article

AN - SCOPUS:0022581676

SN - 0146-3705

JO - AIAA Paper

JF - AIAA Paper

ER -

NUMERICAL SIMULATION OF SEVERAL SHOCK-SEPARATED BOUNDARY-LAYER INTERACTION FLOWS USING ZERO- AND TWO-EQUATION TURBULENCE MODELS.

Abstract

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