0
RESEARCH PAPERS

Measurements of the Turbulent Boundary Layer in the Diffuser Behind an Axial Compressor

[+] Author and Article Information
H. Pfeil, M. Göing

Fachgebiet für Thermische Turbomaschinen, Technische Hochschule Darmstadt, Darmstadt, Federal Republic of Germany

J. Turbomach 109(3), 405-412 (Jul 01, 1987) (8 pages) doi:10.1115/1.3262120 History: Received February 14, 1986; Online November 09, 2009

Abstract

This paper presents boundary layer measurements in a diffuser behind a one-stage axial compressor for the case of nearly axial outlet flow direction from the blades. According to the results, three-dimensional effects caused by the compressor blading have a great influence on the character and development of the turbulent boundary layer and must be included in methods to predict the diffuser flow.

Copyright © 1987 by ASME
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