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TECHNICAL PAPERS

Turbine Nozzle Endwall Film Cooling Study Using Pressure-Sensitive Paint

[+] Author and Article Information
Luzeng J. Zhang

Aero/Thermal and Performance, Solar Turbines, Inc., San Diego, CA 92101

Ruchira Sharma Jaiswal

Development Test, Solar Turbines, Inc., San Diego, CA 92101

J. Turbomach 123(4), 730-738 (Feb 01, 2001) (9 pages) doi:10.1115/1.1400113 History: Received February 01, 2001
Copyright © 2001 by ASME
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References

Figures

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Schematic of scaled cascade test rig
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Double row of hole injection geometry
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Slot injection geometry
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Endwall flow passage, viewing from leading edge direction
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Endwall flow passage, viewing from trailing edge direction
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Film effectiveness distribution on endwall surface, viewed from upstream hole injection
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Film effectiveness distribution on endwall surface, viewed from downstream hole injection
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Film effectiveness distribution on endwall surface, viewed from upstream slot injection
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Film effectiveness distribution on endwall surface, viewed from downstream slot injection
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Circumferential film effectiveness distribution, X/Cax=0, leading edge hole injection
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Circumferential film effectiveness distribution, X/Cax=0, leading edge slot injection
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Circumferential film effectiveness distribution, X/Cax=1.0, trailing edge hole injection
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Circumferential film effectiveness distribution, X/Cax=1.0, trailing edge slot injection
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Circumferential averaged film effectiveness, X/Cax=0 and 1.0, slot and hole injections

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