Hostname: page-component-586b7cd67f-vdxz6 Total loading time: 0 Render date: 2024-11-25T01:41:05.915Z Has data issue: false hasContentIssue false
  • English
  • Français

Theoretical and Experimental Studies of Stall Propagation in Rows of Axial Flow Compressor Blades

Published online by Cambridge University Press:  07 June 2016

M. D. Wood
M. D. Wood*
Affiliation:
University Engineering Laboratory, Cambridge
Get access

Extract

The paper concerns a phenomenon which occurs in rows of closely spaced blades, as in an axial flow compressor, when the flow around the blades approaches the stalling condition. Patches of stalled flow can propagate along the blade row, thus causing cyclic variations in the lift on individual blades. Under certain conditions this cyclic loading can lead to large blade stresses, and ultimately to blade failure.

Type
Research Article
Information
Aeronautical Quarterly , Volume 10 , Issue 4 , November 1959 , pp. 345 - 360
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. Smith, A. G. and Fletcher, P. J. Note on the Surging of Four Low Speed Fans. Internal Note, National Gas Turbine Establishment, 1949.Google Scholar
2. Emmons, H. W., Pearson, C. E. and Grant, H. P. Compressor Surge and Stall Propagation. Paper No. 53-A-65 American Society of Mechanical Engineers Annual Meeting, November 1953.Google Scholar
3. Iura, T. and Rannie, W. D. Experimental Investigations of Propagating Stall in Axial Flow Compressors. Transactions of the American Society of Mechanical Engineers, Vol. 76, No. 3, April 1954.Google Scholar
4. Sears, W. R. On Asymmetric Flow in an Axial Flow Compressor Stage. Journal of Applied Mechanics, Vol. 20, No. 1, March 1954.Google Scholar
5. Marble, F. E. Propagation of Stall in a Compressor Blade Row. Technical Report No. 4, Guggenheim Jet Propulsion Centre, California Institute of Technology, January 1954.Google Scholar
6. Stenning, A. A. Stall Propagation in Cascades of Aerofoils. Readers’ Forum, Journal of the Aeronautical Sciences, Vol. 21, October 1954.Google Scholar
7. Rhoden, H. G. Effects of Reynolds Number on the Flow of Air Through Cascades of Axial Flow Compressor Blades. R. & M. 2919, June 1952.Google Scholar