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A Further Sequel to Technical Note 14: The FUGA Family of Elements for Folded Plate Structures

Published online by Cambridge University Press:  04 July 2016

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

The success of the TUBA plate elements, has not only engendered the development of the SHEBA elements but has also lead, nolens volens, to the consideration of folded plate structures (Faltwerke), which are of considerable practical importance. A little thought shows that a consistent theory of such systems requires that the kinematic representation or interpolation rule of the membrane state is identical to that for the bending state laid down in the TUBA analysis. Moreover, the membrane modes must be effectively the same as the ones adopted for the SHEBA element.

Type
Technical Notes
Information
The Aeronautical Journal , Volume 73 , Issue 703 , July 1969 , pp. 594 - 602
Copyright
Copyright © Royal Aeronautical Society 1969 

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References

1. Argyris, J. H., Fried, I. and Scharpf, D. W. The TUBA Family of Elements for the Matrix Displacement Method. The Aeronautical Journal of the Royal Aeronautical Society, Vol 72, No 692, pp 701–709, August 1968.Google Scholar
2. Argyris, J. H. and Buck, K. E. A Sequel to Technical Note 14 on the TUBA Family of Plate Elements. The Aeronautical Journal of the Royal Aeronautical Society, Vol 72, No 695, pp 977–983, November 1968.Google Scholar
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4. Wittrick, W. H. General Sinusoidal Stiffness Matrices for Buckling and Vibration Analyses of Thin Flat Walled Structures. International Journal of Mechanical Sciences, Vol 10, pp 949–966, 1968.Google Scholar
5. Wittrick, W. H. and Curzon, P. L. V. Stability Functions for the Local Buckling of Thin Flat Walled Structures with the Walls in Combined Shear and Compression. Aeronautical Quarterly, Vol 19, pp 327–351, November 1968.Google Scholar