Choking Effects in the Blade Rows of Turbomachines

J. Horlock
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引用次数: 2

Abstract

Three-dimensional flows through cascades of blades are studied, the blading being fully choked internally. Initially the two-dimensional flow through a ‘zero stagger, zero camber’ blade row, with subsonic entry and exit flow, is described. The radial flows are produced by radial variations in throat area, or by a variety of entry shear flows. Subsequently, the analysis is developed to describe similar fully choked flows through staggered blade rows, particularly the first rotating row of a transonic compressor.
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涡轮机械叶片排中的呛流效应
研究了叶片内部完全堵塞时叶片叶栅内的三维流动。首先,描述了通过“零交错,零弧度”叶片排的二维流动,具有亚音速的入口和出口流动。径向流是由喉道面积的径向变化或各种入口剪切流产生的。随后,分析发展到描述通过交错叶片排,特别是跨音速压气机的第一个旋转排的类似的完全堵塞流动。
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