Hostname: page-component-cd9895bd7-dk4vv Total loading time: 0 Render date: 2024-12-28T20:04:51.206Z Has data issue: false hasContentIssue false
  • English
  • Français

Compressor Design

Published online by Cambridge University Press:  28 July 2016

R. G. Taylor
Get access Rights & Permissions [Opens in a new window]

Extract

In Mr. J. M. Stephenson's Technical Note, “ The Elimination of Wall Effects in Axial-Flow Compressor Stages,” in the April 1953 issue of the Journal, the author suggests that the blade rows of an axial flow compressor are so closely spaced as to ensure that the axial velocity profile is unchanged across the rows. Whether this statement is correct or not such an assumption regarding the axial velocity profile is a basic design condition and when made it will not leave any flexibility in the choice of the function f(r).

Type
Technical Notes
Information
The Aeronautical Journal , Volume 57 , Issue 511 , July 1953 , pp. 463
Copyright
Copyright © Royal Aeronautical Society 1953

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)