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Finite elements for honeycomb sandwich plates and shells*

Part 2: Numerical results and testing

Published online by Cambridge University Press:  04 July 2016

P. J. Holt  and
J. P. H. Webber
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Extract

The general theory and formulation of Part 1 can be applied to a whole family of element shapes. However, quadrilaterals and triangles which are compatible with each other are found to be most useful in idealising general structures. The lowest order polynomial shapes of this kind which are generally curved are the ‘biquadratic’ quadrilateral and the ‘quadratic’ triangle. These have nodes (or nodal pairs for the sandwich elements) situated at the corners and the mid-sides of the ‘parent’ elements. The quadrilateral therefore has eight nodal pairs.

Type
Technical Notes
Information
The Aeronautical Journal , Volume 84 , Issue 832 , May 1980 , pp. 157 - 167
Copyright
Copyright © Royal Aeronautical Society 1980 

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Footnotes

†

The authors: P. J. Holt, formerly British Aerospace Aircraft Group, Weybridge-Bristol Division, now CEGB, Berkeley, Gloucestershire. Dr. J. P. H. Webber, Department of Aeronautical Engineering, University of Bristol.

*

Part 1 was published in the March/April issue of The Aeronautical Journal.

References

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