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Pseudo-Radial Equilibrium in Flared Annuli

Published online by Cambridge University Press:  07 June 2016

J. H. Horlock
J. H. Horlock*
Affiliation:
Department of Mechanical Engineering, Liverpool University
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Summary

A simple method of calculating the flow in turbo-machines with flared annuli is given. Approximate solutions are derived for the compressible swirling flow between the blade rows. Originally received February 1964.

Information

Type
Research Article
Information
Aeronautical Quarterly , Volume 16 , Issue 1 , February 1965, pp. 83 - 91
Copyright
Copyright © Royal Aeronautical Society. 1965

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References

1. Wu, C. H. A General Theory of Three-Dimensional Flow in Subsonic and Supersonic Turbo-Machines of Axial, Radial and Mixed Flow Types. N.A.C.A. T.N. 2604, 1952.Google Scholar
2. Lewis, R. I. and Horlock, J. H. Shear Flows in Straight-Sided Nozzles and Diffusers. International Journal of Mechanical Sciences, Vol. 2 p. 251, 1961.Google Scholar
3. Horlock, J. H. and Lewis, R. I. Non-Uniform Three-Dimensional and Swirling Flows through Diverging Ducts and Turbo-Machines. International Journal of Mechanical Sciences, Vol. 3 p. 170, 1961.Google Scholar
4. Walker, C. P. Compressible Shear Flows in Straight-Sided Nozzles. A.R.C. 23,819, 1962.Google Scholar
5. Horlock, J. H. The Compressible Flow through Cascade Actuator Discs. Aeronautical Quarterly, Vol. IX p. 110, May 1958.Google Scholar
6. Bragg, S. L. and Hawthorne, W. R. Some Exact Solutions of the Flow through Annular Cascade Actuator Discs. Journal of the Aeronautical Sciences, Vol. 17, No. 4, 1950.Google Scholar
7. Horlock, J. H. Axial Flow Compressors. Butterworths, London, 1958.Google Scholar