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On the Tension Loads in Rivets connecting Stringers to Shear-Buckled Skin

Published online by Cambridge University Press:  04 July 2016

E. H. Mansfield
E. H. Mansfield*
Affiliation:
Royal Aircraft Establishment, Farnborough
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Extract

This note derives an approximate, theoretical formula for the tension rivet loads transmitted by a shear-buckled skin to the supporting stringers. Allowance is made for the influence of the in-plane stiffness of the stringers and frames in reducing the magnitude of the shear buckles. The formula will be most reliable in the range 1·5 <τ/τcr< 3. When τ/τcr<1·5 the effect of initial irregularities is important, though the rivet loads are not high. When τ/τcr>3 the effect of change of buckle pattern, neglected in this simplified treatment, becomes important. The analysis could however be extended to deal with varying buckle pattern.

Type
Technical Notes
Information
The Aeronautical Journal , Volume 65 , Issue 601 , January 1961 , pp. 59 - 60
Copyright
Copyright © Royal Aeronautical Society 1961

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References

1.Mansfield, E. H. (1952). On the Post-Buckling Behaviour of Stiffened Plane Sheet Under Shear. R. & M. 3073, 1952.Google Scholar