A two-component LDV was used in a cold flow dump combustor model to obtain detailed mean and turbulence data for both swirling and nonswirling inlet flows. Large samples were collected to resolve the second and third-order products of turbulent fluctuations with good accuracy. Particle interarrival time weighting was used to remove velocity bias from the data. The swirling flows, with and without vortex breakdown, exhibited significantly different mean flow and turbulent field behavior. A numerical scheme with the k–ε closure model was used to predict the flow fields. Comparison of the numerical and experimental results showed that the k–ε turbulence model is inadequate in representing the complex turbulent structure of confined swirling flows.
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January 1989
Research Papers
Application of Laser Velocimetry for Characterization of Confined Swirling Flow
A. S. Nejad,
A. S. Nejad
Aero Propulsion Laboratory, Wright-Patterson AFB, OH 45433
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S. P. Vanka,
S. P. Vanka
Argonne National Laboratory, Argonne, IL
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S. C. Favaloro,
S. C. Favaloro
Aero Propulsion Laboratory, Wright-Patterson AFB, OH 45433
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M. Samimy,
M. Samimy
Department of Mechanical Engineering, Ohio State University, Columbus, OH 43210
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C. Langenfeld
C. Langenfeld
Department of Mechanical Engineering, Ohio State University, Columbus, OH 43210
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A. S. Nejad
Aero Propulsion Laboratory, Wright-Patterson AFB, OH 45433
S. P. Vanka
Argonne National Laboratory, Argonne, IL
S. C. Favaloro
Aero Propulsion Laboratory, Wright-Patterson AFB, OH 45433
M. Samimy
Department of Mechanical Engineering, Ohio State University, Columbus, OH 43210
C. Langenfeld
Department of Mechanical Engineering, Ohio State University, Columbus, OH 43210
J. Eng. Gas Turbines Power. Jan 1989, 111(1): 36-45 (10 pages)
Published Online: January 1, 1989
Article history
Received:
September 10, 1987
Online:
October 15, 2009
Citation
Nejad, A. S., Vanka, S. P., Favaloro, S. C., Samimy, M., and Langenfeld, C. (January 1, 1989). "Application of Laser Velocimetry for Characterization of Confined Swirling Flow." ASME. J. Eng. Gas Turbines Power. January 1989; 111(1): 36–45. https://doi.org/10.1115/1.3240225
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