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Part 1. General Description and Comments on CLmax and Stalling Behaviour

Published online by Cambridge University Press:  04 July 2016

D. M. McRae
D. M. McRae*
Affiliation:
Hawker Siddeley Aviation Ltd, Hatfield
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Extract

The purpose of this paper is to outline briefly the aerodynamics of high-lift devices in the most general possible way to provide the background against which the more detailed advances in calculation methods to be described by the RAE may be viewed. At the same time it is intended to discuss the factors affecting maximum lift coefficient in which the methods described in the RAE paper may be used to obtain improved performance.

Type
Supplementary Papers
Information
The Aeronautical Journal , Volume 73 , Issue 702 , June 1969 , pp. 535 - 541
Copyright
Copyright © Royal Aeronautical Society 1969 

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References

1. Abbott, von Doenhoff and Stivers, . Summary of Airfoil Data. NACA ACR L5C05 Part III. Also published as: Abbott and von Doenhoff. Theory of Wing Sections. McGraw-Hill Book Company Inc, New York.Google Scholar
2. Wilkinson, D. H. Unpublished work at Hawker Siddeley Aviation Ltd, Hatfield.Google Scholar
3. Royal Aeronautical Society Data Sheets. Aerodynamics, Vol. 4, Controls 01.01.03, and Vol. 2, Wings 01.01.05.Google Scholar