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Aston University

The Performance of Aerofoil Cascades Using Circulation Control

Abstract

dc:description.abstract

The performance of a cascade of two-dimensional, bluff aerofoils employing circulation control by a tangential blowing jet is investigated. Expressions for the lift and drag of such a cascade are derived to eliminate the direct effect of the blowing jet on the measured performance. The cascade characteristics for three cascade geometries over a range of incidences are presented as graphs of lift and drag coefficients and stream deflection plotted as functions of jet blowing momentum coefficient. All cascade tests were performed at a Mach number of 0.3. The cascade performance is found to be influenced strongly by vortex shedding at low jet blowing rates. A complete numerical solution procedure for calculating the performance of circulation controlled aerofoils, either isolated or in cascade, is presented. The procedure involves the calculation of a blade surface pressure distribution using a potential flow model with a representation of the separated region by the use of a source distribution. Aerofoil surface boundary layer developments are calculated by a finite-difference solution of the parabolic boundary layer momentum equation. The blowing jet development is calculated by the same finite-difference procedure applied to an angular momentum equation, using an intermittency representation of the eddy viscosity distribution. Results of the solution procedure are compared with experimental results obtained by other workers for an isolated aerofoil and for a cascade. The agreement is satisfactory and encouraging. The solution procedure is applied to two of the cascade configurations tested in the present investigation. The agreement between theory and experiment is excellent in one case, while the poorer agreement in the second comparison is attributed to the experimentally observed changes in wake flow characteristics with cascade geometry.

Degree

thesis:*
Name dc:type.qualificationname
Ph.D.
Level dc:type.qualificationlevel
doctoral
Grantor dc:publisher.institution
Aston University
Year dc:date.issued
1979

Author and committee

dc:creator, dc:contributor.*
Author dc:creator
  • Holliday, C.I.

Identifiers

dc:identifier.*
OAI identifier oai:identifier
oai:publications.aston.ac.uk:11783

Chain of custody

source
Harvested from
Aston University
Base URL
publications.aston.ac.uk/cgi/oai2
Last updated
2026-07-24
Source record
OAI-PMH GetRecord
related terms
citation

Holliday, C.I.. The Performance of Aerofoil Cascades Using Circulation Control. doctoral thesis, Aston University, 1979. https://doi.org/10.48780/publications.aston.ac.uk.00011783