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Two-dimensional compressible flow in centrifugal compressors with straight blades
"Six numerical examples are presented for steady, two-dimensional, compressible, nonviscous flow in centrifugal compressors with thin straight blades, the center lines of which generate the surface of a right circular cone when rotated about the axis of the compressor. A seventh example is presented for incompressible flow. The solutions were obtained in a region of the compressors, including the impeller tip, that was considered to be unaffected by the diffuser vanes or by the impeller-inlet configuration" (p. 141).
Date:
June 21, 1949
Creator:
Stanitz, John D. & Ellis, Gaylord O.
System:
The UNT Digital Library