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TECHNICAL PAPERS

Analysis of the Interrow Flow Field Within a Transonic Axial Compressor: Part 1—Experimental Investigation

[+] Author and Article Information
Xavier Ottavy, Isabelle Trébinjac, André Vouillarmet

Ecole Centrale de Lyon, Laboratoire de Mécanique des Fluides et d’Acoustique, UMR CNRS 5509/ECL/UCB Lyon I, 69131 Ecully Cedex, France

J. Turbomach 123(1), 49-56 (Feb 01, 2000) (8 pages) doi:10.1115/1.1328085 History: Received February 01, 2000
Copyright © 2001 by ASME
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References

Figures

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Time evolutions of mean absolute velocity and standard deviation at a point located on surface B, in a wake-free region, 5 percent of rotor chord upstream of leading edge of rotor
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Flow deceleration through shock in section A, for different blade pitch partitions
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Contour maps on surface B of the standard deviation σV for four different relative positions of rotor blade row
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Contour maps on surface B of the absolute angle α for four different relative positions of rotor blade row
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Contour maps on surface B of the absolute velocity V for four different relative positions of rotor blade row
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Comparison of time-averaged absolute angle fields obtained in section A with L2F and “three-hole” pressure probe
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Comparison of time-averaged absolute velocity fields obtained in section A with L2F and “three-hole” pressure probe
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Contour maps in section A of velocity standard deviation σV for four different positions of rotor blade row
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Contour maps in section A of absolute angle α for four different positions of rotor blade row
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Contour maps in section A of the absolute velocity V for four different positions of rotor blade row
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Experimental mesh of surfaces A and B
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Comparison of measured optical depths of field of anemometer with and without windows
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Optical distortions of a laser cone passing through windows
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Schematic arrangement of optical setup
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Sketch of ECL4 compressor stage

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