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Abstracts from the Scientific and Technical Press, No. 101, April, 1942

Published online by Cambridge University Press:  28 July 2016

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Abstract

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Abstract
Copyright
Copyright © Royal Aeronautical Society 1942

References

Note on page 172 * σorig= stress withstood by undrilkd specimen.

σn=ditto when drilled.

σB=tensile strength of material.

Note on page 174 * S = stress range.

N=Number of cycles.

Note on page 176 * e = eccentricity of loading.

c = distance of extreme filament from neutral axis.

r = radius ,of gyration of cross-section of column.

Note on page 164, 192 * Abstract Available.