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The Stiffness of a Two-Cell Anisotropic Tube

Published online by Cambridge University Press:  07 June 2016

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

An analysis is made of the general two-cell thin-walled cylindrical tube subjected to longitudinal tension, bending and torsion. The walls of the tube may be of fibre composite with an asymmetric lay-up resulting in a coupling between direct and shear stresses and strains. The two-cell tube differs from the single-cell tube in that the tension axis and the principal axes of bending are not necessarily aligned to the c.g. and the principal moments of inertia of the longitudinal stress bearing material.

Type
Research Article
Copyright
Copyright © Royal Aeronautical Society. 1981

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References

1 Mansfield, E.H. and Sobey, A.J. The fibre composite helicopter blade. Aeronautical Quarterly, May 1979 Google Scholar
2 Tsai, S.W. Mechanics of composite materials. Part II, Technical Report AFML-TR-66-149 (1966)Google Scholar
3 Ashton, J.E., Halpin, J.C. and Petit, P.H. Primer on composite materials: analysis. Technomic Publishing Co. (1969)Google Scholar
4 Sechler, E.E. and Dunn, L.G. Airplane structural analysis and design. Galcit Aeronautical Series. John Wiley & Sons, Inc. (1947)Google Scholar
5 Williams, D. The theory of aircraft structures. Edward Arnold Ltd. (1960)Google Scholar