0
RESEARCH PAPERS

Inlet Flow Angle Determination of Transonic Compressor Cascades

[+] Author and Article Information
W. Steinert, R. Fuchs, H. Starken

Deutsche Forschungsanstalt für Luft-und Raumfahrt e.V., Institut für Antriebstechnik, 5000 Köln 90, Federal Republic of Germany

J. Turbomach 114(3), 487-493 (Jul 01, 1992) (7 pages) doi:10.1115/1.2929169 History: Received March 04, 1991; Online June 09, 2008

Abstract

Tests of transonic compressor cascades require special measuring techniques to determine the inlet flow angle around sonic inlet flow conditions. One of the main requirements for these methods is the ability to adjust the inlet flow angle during the test to a prescribed value. A method has been successfully applied that relies on theoretically determined suction surface velocities. The described method was applied in testing cascades at inlet Mack numbers between M1 = 0.75−1.18. The test results confirmed the practicability of this method.

Copyright © 1992 by The American Society of Mechanical Engineers
Your Session has timed out. Please sign back in to continue.

References

Figures

Tables

Errata

Discussions

Some tools below are only available to our subscribers or users with an online account.

Related Content

Customize your page view by dragging and repositioning the boxes below.

Related Journal Articles
Related eBook Content
Topic Collections

Sorry! You do not have access to this content. For assistance or to subscribe, please contact us:

  • TELEPHONE: 1-800-843-2763 (Toll-free in the USA)
  • EMAIL: asmedigitalcollection@asme.org
Sign In