Affiliation:
1. Gas Dynamics Institute, Göttingen, Germany
Abstract
This paper deals with the flow through cascades, which have a supersonic flow up- and downstream. A theoretical method is described to calculate, under certain conditions, the flow quantities up- and downstream of and within the cascade and to determine the pressure distribution on the blades. The method is compared with experimental results, carried out in the cascade wind tunnel of the Aero dynamische Versuchsanstalt Göttingen (AVA), Germany.
Publisher
American Society of Mechanical Engineers
Cited by
4 articles.
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