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Initial buckling of lipped channel struts

Published online by Cambridge University Press:  04 July 2016

F. W. Williams
F. W. Williams*
Affiliation:
Department of Civil Engineering, University of Birmingham
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Extract

Several recent theoretical advances have been incorporated in computer programs which find the initial buckling loads of prismatic assemblies of thin plates “exactly”. Any such assembly of plates which are connected together and/or supported along their longitudinal edges, while being simply supported at their ends, can be analysed. Furthermore, curved plates and anistropic materials are allowed. Thus plate assemblies with many practically important types of cross-section can be analysed. Consequently, published results mainly relate to a few crosssections of each of several possible types. However, the designer needs comprehensive design curves, like those in the Structures Data Sheets of the Royal Aeronautical Society, for as many common cross-section types as possible. Unfortunately, production of such curves using the programs mentioned is unlikely to be achieved for all desired types of cross-section, at least for some time, because each type involves plotting curves as several parameters are varied. Nevertheless, a range of results for one type of cross-section is obviously valuable. Thus the lipped channel strut made from isotropic material is considered in this Note (see Fig. 1).

Type
Technical notes
Information
The Aeronautical Journal , Volume 78 , Issue 766 , October 1974 , pp. 468 - 475
Copyright
Copyright © Royal Aeronautical Society 1974 

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References

1. Wittrick, W. H. A unified approach to the initial buckling of stiffened panels in compression. Aeronautical Quarterly, Vol XIX, pp 265–283, 1968.Google Scholar
2. Williams, F. W. Computation of natural frequencies and initial buckling stresses of prismatic plate assemblies. Journal of Sound and Vibration, Vol 21, pp 87–106, 1972.Google Scholar
3. Smith, C. S. Bending, buckling and vibration of orthotropic plate-beam structures. Journal of Ship Research, Vol 12, pp 249–268, 1968.Google Scholar
4. Viswanathan, A. V. et al. Elastic stability of biaxially loaded longitudinally stiffened composite structures. Proceedings of the AIAA|ASME|SAE 14th Structures, Structural Dynamics and Materials Conference, Williamsburg, Virginia, March 1973.Google Scholar
5. Wittrick, W. H. and Williams, F. W. Buckling and vibration of anisotropic or isotropic plate assemblies under combined loadings. International Journal of Mechanical Sciences, Vol 16, pp 209–239, 1974.Google Scholar
6. Williams, F. W. and Wittrick, W. H. Numerical results for the initial buckling of some stiffened panels in compression. Aeronautical Quarterly, Vol XXIII, pp 24–40, 1972.Google Scholar
7. Smith, C. S. Buckling problems in the design of fibreglass reinforced plastic ships. Journal of Ship Research, Vol 16, pp 174–190, 1972.Google Scholar
8. Viswanathan, A. V., et al. Buckling analysis for structural sections and stiffened plates reinforced with laminated composites. International Journal of Solids and Structures, Vol 8, p? 347–367, 1972.Google Scholar