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RISDiscussion: “Design of Cascades for Incompressible Plane Potential Flows With Prescribed Velocity Distribution” (Schwering, W., 1971, ASME J. Eng. Power, 93, pp. 321–331)
Publisher: The American Society of Mechanical Engineers (ASME)
Influence of a Closely Coupled Throttle on the Stalling Behavior of a Radial Compressor Stage
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: On the basis of the classical discussion of the stability of compressor blade rows, a treatment is given of the stability of a stage consisting of a radial impeller followed by a vaned ...
A Theory for Boundary Layer Growth on the Blades of a Radial Impeller Including Endwall Influence
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Experimental data on the wall shear stress of a turbulent boundary layer on the suction side of a blade in a two-dimensional radial impeller is compared with the predictions of a theory which ...
Treatment of the Annulus Wall Boundary Layer Using a Secondary Flow Hypothesis
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Hitherto, theories of annulus wall boundary layer development in axial compressors have assumed an axially-symmetric flow in which the blade action has been replaced by a force field. A more ...