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Improvements on the analysis of shells of revolution by the matrix displacement method.

✍ Scribed by NAVARATNA, D. R.; PIAN, T. H. H.; PIAN, T. H. H.; STRICKLIN, J. A.


Book ID
120355680
Publisher
American Institute of Aeronautics and Astronautics
Year
1966
Tongue
English
Weight
483 KB
Volume
4
Category
Article
ISSN
0001-1452

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Shells of revolution subject to axisymmetric loads often fail by non-symmetric bifurcation buckling after non-linear axisymmetric deformations. A number of computer programmes have been developed in the past decades for these problems, but none of them is capable of bifurcation analysis on the desce