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TECHNICAL PAPERS

Wake, Shock, and Potential Field Interactions in a 1.5 Stage Turbine—Part I: Vane-Rotor and Rotor-Vane Interaction

[+] Author and Article Information
R. J. Miller

Whittle Laboratory, University of Cambridge, Cambridge, CB30 DY, UK

R. W. Moss

Department of Marine Technology, University of Newcastle, Newcastle upon Tyne NE1 7RU, UK

R. W. Ainsworth

Department of Engineering Science, University of Oxford, Oxford OX1 3PJ, UK

N. W. Harvey

Rolls Royce plc., Derby DE24 8BJ, UK

J. Turbomach 125(1), 33-39 (Jan 23, 2003) (7 pages) doi:10.1115/1.1508386 History: Received January 31, 2002; Online January 23, 2003
Copyright © 2003 by ASME
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References

Figures

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The two test sections with and without a downstream vane
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Location of pressure sensors
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Photograph of instrumented blade
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Experimental measurement of suction surface static pressure
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Computational prediction of the suction surface static pressure
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(a) Sensor location, (b) schematic of flow structure
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Power spectrum of an idealized rotor surface pressure measurement
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Sensor 6 pressure surface (ensemble average)
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Sensor 6 pressure surface (power spectrum)
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Suction surface pressure sensor 2
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Suction surface pressure sensor 7
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Suction surface pressure sensor 8
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Suction surface sensor 11 (expanded)

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