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A Simple Method for Predicting the Performance of Cascades of Low Solidity

Published online by Cambridge University Press:  07 June 2016

K. Tanabe
Affiliation:
Department of Mechanical Engineering, University of Liverpool
J. H. Horlock
Affiliation:
Department of Mechanical Engineering, University of Liverpool
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Summary

A simple potential theory for flow through cascades of low solidity is developed. The analysis is an extension of Glauert’s theory for single aerofoils. The variation of outlet angle and lift coefficient with space/chord ratio and stagger angle is predicted. The simple analysis is shown, by comparison with other methods of computation, to be valid for cascades of space/chord ratio in excess of 1·5 and staggers over 50 degrees.

Information

Type
Research Article
Copyright
Copyright © Royal Aeronautical Society. 1967

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