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TECHNICAL PAPERS

Viscous-Flow Two-Dimensional Analysis Including Secondary Flow Effects

[+] Author and Article Information
Reinhard Mönig, Frank Mildner

Siemens AG Power Generation KWU Mülheim a. d. Ruhr, Germany

Ralf Röper

B&B-AGEMA GmbH Aachen, Germany

J. Turbomach 123(3), 558-567 (Feb 01, 2000) (10 pages) doi:10.1115/1.1370167 History: Received February 01, 2000
Copyright © 2001 by ASME
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References

Figures

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Model of axial compressor stage with shrouded hub and seal strips
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Compressor cross section three-stage research compressor (Institute for Jet Propulsion and Turbomachinery, Technical University of Aachen)
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Relative whirl angle downstream Rotor 1
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Relative whirl angle downstream Rotor 3
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Absolute whirl angle upstream Stator 1
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Absolute whirl angle upstream Stator 2
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Exit absolute whirl angle (three-stage research compressor)
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Stagnation pressure at compressor exit (three-stage research compressor)
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Relative whirl angle of a rotor in the mid section of the V84.3A compressor
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Relative whirl angle of a rotor at the back end of the V84.3A compressor
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Development of radial total pressure distribution of the V84.3A compressor
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Total temperature rotor 7
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Relative whirl angle rotor 7
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Total temperature rotor 8
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Relative whirl angle rotor 8
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Velocity distributions in boundary layers
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Numerical sublayer thickness for accelerated flows
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Numerical sublayer thickness for decelerated flows

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