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TECHNICAL PAPERS

Influence of Vane/Blade Spacing on the Heat Flux for a Transonic Turbine

[+] Author and Article Information
M. G. Dunn, C. W. Haldeman, R. S. Abhari, M. L. McMillan

The Ohio State University, Gas Turbine Laboratory, Columbus, OH 43235

J. Turbomach 122(4), 684-691 (Feb 01, 2000) (8 pages) doi:10.1115/1.1313818 History: Received February 01, 2000
Copyright © 2000 by ASME
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References

Figures

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Sketch of Allison VBI turbine located in OSU GTL shock tunnel
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General instrumented blade locations on VBI turbine
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Vane time-averaged Nusselt number (20 percent spacing)
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Vane time-averaged Nusselt number (40 percent spacing)
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Vane time-averaged Nusselt number (60 percent spacing)
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Composite plot of vane Nusselt number for different spacings
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Blade time-averaged Nusselt number (20 percent spacing)
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Blade time-averaged Nusselt number (40 percent vane–rotor spacing)
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Blade time-averaged Nusselt number (60 percent spacing)
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Composite plot of blade Nusselt number for different spacings
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Blade suction surface data near stagnation point (20 percent spacing)
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Blade pressure surface data near stagnation point (20 percent spacing)
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Blade pressure surface data (20 percent spacing)
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Blade suction surface data (20 percent spacing)
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Blade suction surface data (20 percent spacing)
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Unsteady Nusselt number envelopes for 20 percent spacing
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Unsteady Nusselt number envelopes for 60 percent spacing

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