Matrix Displacement Analysis of Anisotropic Shells by Triangular Elements
- 1 August 1965
- journal article
- research article
- Published by Cambridge University Press (CUP) in Journal of the Royal Aeronautical Society
- Vol. 69 (659) , 801-805
- https://doi.org/10.1017/s0368393100081827
Abstract
Over the last five years or so both in the USA (especially by the active group at Berkeley under R. W. Clough(7) ) and the UK, there have been a number of attempts to incorporate the plane triangular element under bending and membrane action into a general matrix displacement analysis of shells. All investigators stressed the positive aspects of the triangular element, which arise from its adaptability to any geometrical form of the shell, but noted at the same time some serious shortcomings due to a partial satisfaction of the kinematic compatibility conditions at the boundary. Thus we have within the Matrix Displacement Method the rather unusual example of a type of element whose deficiency with respect to kinematic compatibility does not automatically ensure convergence to the exact result as the number of elements is increased.Keywords
This publication has 3 references indexed in Scilit:
- Matrix displacement analysis of plates and shellsArchive of Applied Mechanics, 1966
- Reinforced Fields of Triangular Elements with Linearly Varying Strain; Effect of Initial StrainsJournal of the Royal Aeronautical Society, 1965
- Three-dimensional anisotropic and inhomogeneous elastic media matrix analysis for small and large displacementsArchive of Applied Mechanics, 1965