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TECHNICAL PAPERS: Internal Combustion Engines

Numerical Study of Nonreacting Gas Turbine Combustor Swirl Flow Using Reynolds Stress Model

[+] Author and Article Information
S. L. Yang, Y. K. Siow, B. D. Peschke

Department of Mechanical Engineering and Engineering Mechanics, Michigan Technological University, 1400 Townsend Drive, Houghton, MI 49931  

R. R. Tacina

Combustion Technology Branch, NASA John H. Glenn Research Center, Lewis Field, 21000 Brookpark Road, Cleveland, OH 44135

J. Eng. Gas Turbines Power 125(3), 804-811 (Aug 15, 2003) (8 pages) doi:10.1115/1.1560706 History: Received February 01, 2002; Revised March 01, 2002; Online August 15, 2003
Copyright © 2003 by ASME
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References

Figures

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Combustor mesh and cutting planes
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A sketch of the swirler
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Results for 60 deg swirler at z=5 mm cutting plane: (a) Reynolds stress turbulence model, (b) k-ε, (c) experiment
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Results for 60 deg swirler at z=11 mm cutting plane: (a) Reynolds stress turbulence model, (b) k-ε, (c) experiment
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Results for 60 deg swirler at z=18 mm cutting plane: (a) Reynolds stress turbulence model, (b) k-ε, (c) experiment
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Velocity on y0-y0 plane for 60 deg swirler: (a) Reynolds stress turbulence model, (b) k-ε
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Velocity on y1-y1 plane for 60 deg swirler: (a) Reynolds stress turbulence model, (b) k-ε
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Results for 45 deg swirler at z=11 mm plane: (a) Reynolds stress turbulence model, (b) k-ε
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RSTM velocity on y0-y0 plane for 45 deg swirler: (a) Reynolds stress turbulence model, (b) k-ε
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Results for 60 deg clockwise and counterclockwise swirler at z=11 mm plane: (a) Reynolds stress turbulence model, (b) k-ε
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RSTM velocity on y0-y0 plane for 60 deg cw+ccw swirler: (a) Reynolds stress turbulence model, (b) k-ε

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