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TECHNICAL PAPERS

The Influence of Technical Surface Roughness Caused by Precision Forging on the Flow Around a Highly Loaded Compressor Cascade

[+] Author and Article Information
Robert Leipold, Matthias Boese, Leonhard Fottner

Institut für Strahlantriebe, Universität der Bundeswehr München, D-85577 Neubiberg, Germany

J. Turbomach 122(3), 416-424 (Feb 01, 1999) (9 pages) doi:10.1115/1.1302286 History: Received February 01, 1999
Copyright © 2000 by ASME
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References

Figures

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High-speed cascade wind tunnel
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NACA 65 K48 cascade mounted in test section
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Three-dimensional topology of applied sheet of copper
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Location of measurement planes
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Influence of Reynolds number on isentropic Mach number
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Influence of Reynolds number on local total pressure loss
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Influence of Reynolds number on total pressure loss coefficient
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Influence of Reynolds number on boundary layer parameters
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Influence of Reynolds number on distribution of turbulence in boundary layer
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Isentropic Mach number and wake traverse results for a variation of inlet angle
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Total pressure loss coefficient difference versus inlet flow angle
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Influence of inlet flow angle on boundary layer parameters
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Influence of inlet flow angle on distribution of turbulence in boundary layer

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