0
RESEARCH PAPERS

Performance Prediction for High Turning Low Aspect Ratio Stator Cascades in the Transonic Regime

[+] Author and Article Information
H. F. L. Griepentrog

von Karman Institute, Rhode St. Genese, Belgium

J. Eng. Power 92(4), 390-398 (Oct 01, 1970) (9 pages) doi:10.1115/1.3445369 History: Received January 19, 1970; Online July 14, 2010

Abstract

This paper describes a method for the prediction of the transonic flow field in a high solidity, high turning cascade, suitable for use as stator of a shock-in-rotor supersonic compressor stage. Effects of shock boundary layer interaction is taken into account by empirical correlation, valid for blade aspect ratios below unity. Use of partial slots for reduction of the secondary flows is briefly discussed and a correlation on slot efficiency is presented.

Copyright © 1970 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