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TECHNICAL PAPERS

Predicting Bladerow Interactions Using a Multistage Time-Linearized Navier-Stokes Solver

[+] Author and Article Information
W. Ning, Y. S. Li, R. G. Wells

ALSTOM Power, UK Ltd., Lincoln LN5 7FD, UK

J. Turbomach 125(1), 25-32 (Jan 23, 2003) (8 pages) doi:10.1115/1.1516570 History: Received January 07, 2002; Online January 23, 2003
Copyright © 2003 by ASME
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References

Figures

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Static pressure distribution on rotor blade surface
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Instantaneous entropy contours
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Instantaneous unsteady velocity vectors
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Unsteady pressure time traces on rotor blade surfaces
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Sketch of DLR transonic counter-rotating propfan
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Sketch of DLR transonic counter-rotating propfan
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Instantaneous pressure contours by linear method
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Instantaneous pressure contours by nonlinear method
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Instantaneous entropy contours by linear method
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Relative velocity and flow angle at axial plane M1
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Unsteady amplitude of relative velocity and flow angle at axial plane M1
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Relative velocity and flow angle at axial plane M2
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Unsteady amplitude of relative velocity and flow angle at axial plane M2
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Relative velocity and flow angle at axial plane M3
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Unsteady amplitude of relative velocity and flow angle at axial plane M3
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Relative velocity and flow angle at axial plane M4
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Unsteady amplitude of relative velocity and flow angle at axial plane M4
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1st harmonic unsteady pressure on blade surface

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