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Part II Elastic Stiffness and Influence of Initial Strains

Published online by Cambridge University Press:  04 July 2016

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Extract

The preparatory work of the preceding technical note is followed up by deriving the elastic stiffness and the initial load vector of an arbitrary TRIAX 6 element subject to an axisymmetric state of stress or strain.

Type
Technical Notes
Information
The Aeronautical Journal , Volume 70 , Issue 672 , December 1966 , pp. 1105 - 1106
Copyright
Copyright © Royal Aeronautical Society 1966

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References

1.Argyris, J. H.The TRIAX 6 Element for Axisymmetric Analysis by the Matrix Displacement Method, Part I Foundations. Journal of the Royal Aeronautical Society, Vol. 70, December 1966.Google Scholar
2.Argyris, J. H. and Spooner, J. B. The Thermoelasto-plastic Analysis of a Re-entry Body Type Composite Solid Structure Using a New Finite Element Development for Axially Symmetric Systems. Paper at XVIIth International Aeronautical Congress, Madrid. 10th-15th October 1966. To be published.Google Scholar