Hostname: page-component-586b7cd67f-dlnhk Total loading time: 0 Render date: 2024-11-24T22:47:50.740Z Has data issue: false hasContentIssue false
  • English
  • Français

Relative Eddy and its Effects on the Performance of a Radial Bladed Centrifugal Impeller

Published online by Cambridge University Press:  28 July 2016

K. R. Reddy
Get access Rights & Permissions [Opens in a new window]

Summary

Mathematical and experimental methods for estimating the relative eddy velocity in a radial bladed impeller channel have been determined to replace the empirical velocity so far used in designing and predetermining the performance. The effect of this relative eddy velocity on rotor performance has been experimentally determined on a specially designed compressor and compared with mathematical calculation.

Type
Research Article
Information
The Aeronautical Journal , Volume 58 , Issue 524 , August 1954 , pp. 547 - 555
Copyright
Copyright © Royal Aeronautical Society 1954

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. Kearton, W. J. (1933). The Influence of the Number of Impeller Blades on the Pressure Generated in a Centrifugal Compressor and its general performance. Proceedings of the Institution of Mechanical Engineers, Vol. 124, p. 481, 1933.CrossRefGoogle Scholar
2. Stodola, A. (1927). Steam and Gas Turbines. McGraw Hill, Vol. II, p. 1,259, 1927.Google Scholar
3. Ainley, D. G. and Bailey, FT./ L T . W. (1944). Note on Cylindrical Yawmeter for Measuring the Static Pressures. R.A.E. Farnborough Tech. Note Eng. 285, 1944.Google Scholar
4. McAdams, W. H. (1942). Heat Transmission. 2nd Edition, McGraw-Hill, Fig. 51, p. 118, 1942.Google Scholar