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TECHNICAL PAPERS

Local Mass/Heat Transfer on Turbine Blade Near-Tip Surfaces

[+] Author and Article Information
P. Jin, R. J. Goldstein

Heat Transfer Laboratory, Department of Mechanical Engineering, University of Minnesota, Minneapolis, MN 55455

J. Turbomach 125(3), 521-528 (Aug 27, 2003) (8 pages) doi:10.1115/1.1554410 History: Received October 10, 2001; Online August 27, 2003
Copyright © 2003 by ASME
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References

Figures

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Planview of the test section
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Cascade blade geometry and balance test—(a) cascade blade geometry, (b) cascade blade balance test data
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Sh contour with zero tip clearance—(a) pressure surface, (b) suction surface
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Sh contour on the pressure surface—(a) t/C=0.86%, (b) t/C=1.72%
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Sh contour on the pressure surface—(a) t/C=3.45%, (b) t/C=6.90%
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Sh/Reex1/2 on the pressure surface
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Average Sh on the pressure surface—(a) spanwise average, (b) streamwise average
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Sh/Reex1/2 on the pressure surface at t/C=0.86%
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Sh contour on the suction surface—(a) t/C=0.86%, (b) t/C=1.72%
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Sh contour on the suction surface—(a) t/c=3.45%, (b) t/C=6.90%
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Sh/Reex1/2 on the suction surface
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Average Sh on the suction surface—(a) spanwise average, (b) streamwise average
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Sh/Reex1/2 on the suction surface at t/C=0.86%

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