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Part II Elastic Stiffness and Influence of Initial Strains

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.

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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.
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.
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The Aeronautical Journal
  • ISSN: 0001-9240
  • EISSN: 2059-6464
  • URL: /core/journals/aeronautical-journal
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