Theory on Blades of Axial, Mixed, and Radial Turbomachines by Inverse Method
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概要
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In this paper, a theory on blades of axial, mixed, and radial turbomachines is presented, in which the shapes of blades are obtained with the prescribed velocity distribution along the blade surfaces. The singularity method is used in this theory; vortices, sources and sinks are arranged along the camber line of blade sections on the mean stream surface of revolution. The effect of three-dimensional flow due to the arbitrary shapes of the mean stream surfaces through blades is also taken into account.
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