Secondary Flow in Cascades: Two Simple Derivations for the Components of Vorticity

Author:

Came P. M.1,Marsh H.2

Affiliation:

1. National Gas Turbine Establishment, Pyestock, Farnborough, Hampshire

2. Professor of Engineering Science, University of Durham, Fellow of the Institution

Abstract

By considering a many-bladed cascade, two simple theories are developed for secondary flow in cascades. Following the work of Hawthorne (1), three components of vorticity are identified at exit from the cascade. An expression is obtained for the difference in the time taken for fluid particles to travel over the two surfaces of the blade, and this is used to derive the governing equations for the distributed secondary, trailing filament and trailing shed vorticities. It is shown that, for a many-bladed cascade, the total secondary circulation in the downstream flow is zero. The calculation of secondary flow for a real cascade is discussed, and it is shown that earlier calculations of secondary flow at exit from cascades are consistent with this new approach.

Publisher

SAGE Publications

Subject

General Engineering

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1. On the Vortical Structures in a Linear Blade Cascade;Topical Problems of Fluid Mechanics 2023;2023

2. Experimental Investigation of Effects of Reynolds Number and Incidence Angle on Secondary Flow within a Linear Blade Cascade;Journal of Thermal Science;2021-10-20

3. The sensitivity of turbine cascade endwall loss to inlet boundary layer thickness;Journal of the Global Power and Propulsion Society;2019-03-26

4. Endwall Loss in Turbine Cascades;Journal of Turbomachinery;2017-03-15

5. Secondary Flow Control and Loss Reduction in a Turbine Cascade Using Endwall Fences;JSME international journal. Ser. 2, Fluids engineering, heat transfer, power, combustion, thermophysical properties;1989

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