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Supersonic Flow in Turbines and Compressors*

Published online by Cambridge University Press:  28 July 2016

K. W. Sorg
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Extract

Whereas a body of theoretical research is available on the conditions of supersonic flow through Laval nozzles and around aerofoils, such is lacking for turbo-machinery in general, with the exception of some researches by Stodola, confined to axial steam turbines. The present paper investigates some important questions relating to the flow at supersonic velocity through centrifugal machines of the general type.

Type
Research Article
Information
The Aeronautical Journal , Volume 46 , Issue 375 , March 1942 , pp. 64 - 85
Copyright
Copyright © Royal Aeronautical Society 1942

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Footnotes

*

R.T.P. Translation. Published by permission of the Ministry of Aircraft Production.

References

Note on page No 64 † A. Stodola. “ Dampf-und Gasturbinen ” (“ Steam and Gas Turbines ” ) . 6th Ed., Berlin 1924, pp. 131 et seq, p. 809 et seq.

Note on page No 70 * The initial condition has been specified as u = o in order to simplify calculation

Note on page No 77 * A. Busemann. “ Gasdynamik, Handbueh der Exp.-Physik ” (Gas Dynamics, Handbook of Experimental Physics), Vol. IV, 1, Leipzig 1931.

Note on page No 80 * Lamb, H.. “ Lehrbuch der Hydrodynamik ” (“ Handbook of Hydrodynamics ”). 2nd Ed., Leipzig, Berlin 1931.Google Scholar

Note on page No 81 * Lamb, H.. “ Lehrbuch der Hydrodynamik ” (“ Handbook of Hydrodynamics ”). 2nd Ed., Leipzig, Berlin 1931.Google Scholar

Note on page No 82 * Lamb, H.. “ Lehrbuch der Hydrodynamik ” (“ Handbook of Hydrodynamics ”). 2nd Ed., Leipzig, Berlin 1931.Google Scholar

Note on page No 83 * The extent to which the derived relations are modified by a finite number of blades, will not be further dealt with.