Spatial Supersonic Flow Through Annular Cascades

[+] Author and Article Information
H. H. Fruehauf

Institut für Raumfahrtantriebe, Universität Stuttgart, D 7000 Stuttgart 80, Pfaffenwaldring 31, Germany

J. Eng. Power 98(2), 274-280 (Apr 01, 1976) (7 pages) doi:10.1115/1.3446163 History: Received December 13, 1974; Online July 14, 2010


The spatial supersonic flow through rotating and stationary annular cascades is analyzed by means of a nonlinear three-dimensional method of characteristics. Three-dimensional corrections for flow quantities referred to a quasi-three-dimensional approximation method are determined depending on geometric and gas dynamical parameters. Characteristic properties of spatial supersonic flow through annular cascades are analyzed, leading to guiding principles for practical design purposes.

Copyright © 1976 by ASME
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