Secondary Flow in Cascades: Two Simple Derivations for the Components of Vorticity
- 1 December 1974
- journal article
- research article
- Published by SAGE Publications in Journal of Mechanical Engineering Science
- Vol. 16 (6) , 391-401
- https://doi.org/10.1243/jmes_jour_1974_016_073_02
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.Keywords
This publication has 4 references indexed in Scilit:
- ROTATIONAL FLOW THROUGH CASCADES PART I. THE COMPONENTS OF VORTICITYThe Quarterly Journal of Mechanics and Applied Mathematics, 1955
- ROTATIONAL FLOW THROUGH CASCADES PART II. THE CIRCULATION ABOUT THE CASCADEThe Quarterly Journal of Mechanics and Applied Mathematics, 1955
- A Simple Approach to the Theory of Secondary FlowsAeronautical Quarterly, 1954
- The Secondary Flow in a Cascade of Airfoils in a Nonuniform StreamJournal of the Aeronautical Sciences, 1951