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The Optimum Design of Compression Surfaces having Unflanged Integral Stiffeners

Published online by Cambridge University Press:  28 July 2016

E. J. Catchpole
E. J. Catchpole*
Affiliation:
Vickers-Armstrongs Ltd., Weybridge
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Summary

A method is developed enabling rapid determination of the optimum cross-sectional dimensions of compression surfaces having unflanged integral stiffeners, and consideration is given to the effects of practical limitations on the design. The theoretical efficiency of the optimum integral design is found to be only 85 per cent, of that of optimum Z-stringer design.

Information

Type
Research Article
Information
The Aeronautical Journal , Volume 58 , Issue 527 , November 1954 , pp. 765 - 768
Copyright
Copyright © Royal Aeronautical Society 1954

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References

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