Hostname: page-component-78c5997874-dh8gc Total loading time: 0 Render date: 2024-11-10T05:27:17.144Z Has data issue: false hasContentIssue false
  • English
  • Français

Wakes in Axial Compressors

Published online by Cambridge University Press:  04 July 2016

W. F. Wiles
W. F. Wiles*
Affiliation:
Aero Engine Division, Rolls-Royce Ltd.
Get access Rights & Permissions [Opens in a new window]

Extract

The note in the July Journal by H. Pearson and A. B. McKenzie (p. 415) shows that the flow into an axial compressor is nearly at a constant velocity at all points in the entry plane; and that if a wake of low energy air is fed into it, the compressor reduces the static pressure locally in this wake, in such a way as to tend to preserve constant velocity over the whole face.

Type
Technical Notes
Information
The Aeronautical Journal , Volume 63 , Issue 588 , December 1959 , pp. 730 - 731
Copyright
Copyright © Royal Aeronautical Society 1959

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.)

References

1.Alford, J. S. (1957). Inlet Flow Distortion Index. Paper presented at the International Days of Aeronautical Sciences, Paris, 27th-29th May 1957.Google Scholar
2.Greatrex, F. B. (1954). Air Intake Efficiency. Journal of the Royal Aeronautical Society, Vol. 58, Sept. 1954.Google Scholar