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A general computer solution for radial and mixed flow turbomachine performance prediction

โœ Scribed by A. Whitfield; N.C. Baines


Publisher
Elsevier Science
Year
1976
Tongue
English
Weight
409 KB
Volume
18
Category
Article
ISSN
0020-7403

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A technique is described for the analytical representation of the geometry of radial a~ld mixed flow compressor impellers constructed of radial or non-radial blade elements. A similar analytical expression is used to describe the hub, shroud, and camberline curves; if required, the angle of inclinat