The Compressible Flow Through Cascade Actuator Discs

Author:

Horlock J. H.

Abstract

SummaryA theory of the incompressible flow through two- and three-dimensional cascade actuator discs has been developed by several workers over the past ten years, and its accuracy has been confirmed in several experiments. This theory is briefly reviewed, and a parallel theory for subsonic compressible flow through actuator discs is developed. Approximate solutions for several examples are considered, including a compressible shear flow through a two-dimensional cascade, and a compressible flow through an annular cascade of guide vanes.

Publisher

Cambridge University Press (CUP)

Subject

General Engineering

Reference13 articles.

1. Horlock J. H. and Carmichael A. D. Actuator Disc Theories Applied to the Design of Axial Compressors. A.R.C. Current Paper 315,1957.

2. Horlock J. H. Experimental and Theoretical Investigations of the Flow of Air through Two Single Stage Compressors. R. & M. 3031, 1955.

3. Some Exact Solutions of the How through Annular Cascade Actuator Discs;Bragg;Journal of the Aeronautical Sciences,1950

4. Hawthorne W. R. Three Dimensional Flow in Compressors. Westinghouse Internal Report (unpublished), 1950.

5. The Flow of a Perfect Fluid through an Axial Flow Turbo Machine with Pre-described Blade Loading;Marble;Journal of the Aeronautical Sciences,1948

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1. Choking Effects in the Blade Rows of Turbomachines;Journal of Mechanical Engineering Science;1980-08

2. Compressible Shear Flows in the Duct with Varying Cross-Sectional Area;The Journal of the Royal Aeronautical Society;1967-02

3. Pseudo-Radial Equilibrium in Flared Annuli;Aeronautical Quarterly;1965-02

4. A theoretical investigation of the rotational flow of incompressible fluids through axial turbo-machines with tapered annulus walls;International Journal of Mechanical Sciences;1964-02

5. Paper 5: Actuator Disc Theory of the Compressible Flow in Free-Vortex Turbo-Machinery;Proceedings of the Institution of Mechanical Engineers, Conference Proceedings;1963-06

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