0
RESEARCH PAPERS

The Influence of Tip Clearance on Stall Limits of a Rectilinear Cascade of Compressor Blades

[+] Author and Article Information
Ghassan Khabbaz

Applied Mechanics Laboratory, Massachusetts Institute of Technology, Cambridge, Mass.

Yasutoshi Senoo

Massachusetts Institute of Technology, Cambridge, Mass.

J. Basic Eng 83(3), 371-377 (Sep 01, 1961) (7 pages) doi:10.1115/1.3658967 History: Received August 02, 1960; Online November 04, 2011

Abstract

An experimental study of the influence of tip clearance on the stall limits of compressor blades was conducted on a rectilinear cascade. By using the mirror and image technique the end wall boundary layer near the clearance was dispensed with. The blade loading was maximum at a distance from the tip clearance, but the clearance was found to relieve the pressure gradient in general and to retard stalling.

Copyright © 1961 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