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The Hermes 8 Element for the Matrix Displacement Method

Published online by Cambridge University Press:  04 July 2016

J. H. Argyris ,
I. Fried  and
D. W. Scharpf
J. H. Argyris
Affiliation:
Imperial College of Science and Technology, University of London Institut für Statik und Dynamik der Luft-und Raumfahrtkonstruktionen, Universität Stuttgart
I. Fried
Affiliation:
Imperial College of Science and Technology, University of London Institut für Statik und Dynamik der Luft-und Raumfahrtkonstruktionen, Universität Stuttgart
D. W. Scharpf
Affiliation:
Imperial College of Science and Technology, University of London Institut für Statik und Dynamik der Luft-und Raumfahrtkonstruktionen, Universität Stuttgart
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Extract

The description of the LUMINA element in T.N. 11 is followed by another three-dimensional interpolation element, called HERMES 8, available in the ASKA language and briefly mentioned in ref. 1. Just as the LUMINA set, the HERMES element represents a general hexahedronal element with curved faces and has proved a most useful component block for three-dimensional analysis of complex bodies. The cardinal idea underlying the HERMES development aims at combining the advantages of the Lagrangian and Hermitian interpolation techniques.

Information

Type
Technical Notes
Information
The Aeronautical Journal , Volume 72 , Issue 691 , July 1968 , pp. 613 - 617
Copyright
Copyright © Royal Aeronautical Society 1968 

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References

1. Argyris, J. H. The Computer Shapes the Theory, Lecture to the Royal Aeronautical Society, 19th May 1965. To be published in The Aeronautical Journal of the Royal Aeronautical Society.Google Scholar
2. Argyris, J. H., Fried, I. The LUMINA Element for the Matrix Displacement Method, (TN 11). The Aeronautical Journal of the Royal Aeronautical Society, Vol 72, No 690, pp 514–517, June 1968.Google Scholar