1984
DOI: 10.1115/1.3167642
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Divergence of Cantilever Columns Under Combined Conservative and Follower Loads

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Cited by 4 publications
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“…The methods of loading the system which have an influence on the type of stability loss (divergence or flutter) are as follows: Beck's generalized load (a load generated by an under-follower force) (Gajewski, 2001;Herrmann and Bungay, 1964;Ryu et al, 2000;Sato, 1996;Smith and Herrman, 1972;Tomski and Przybylski, 1985;Tomski et al, 2007) and a load generated by the simultaneous performance of a conservative (axial) and non-conservative load (follower -Beck's) (Flax, 1984;Hernández-Urrea and Dario Aristizabal-Ochoa, 2008;Langthjem and Sugiyama, 2000;Ryu et al, 2000;Sugiyama et al, 2000). Beck's generalized load, considered in this paper, is a load for which the direction of the force is determined by the follower coefficient.…”
Section: Introductionmentioning
confidence: 99%
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“…The methods of loading the system which have an influence on the type of stability loss (divergence or flutter) are as follows: Beck's generalized load (a load generated by an under-follower force) (Gajewski, 2001;Herrmann and Bungay, 1964;Ryu et al, 2000;Sato, 1996;Smith and Herrman, 1972;Tomski and Przybylski, 1985;Tomski et al, 2007) and a load generated by the simultaneous performance of a conservative (axial) and non-conservative load (follower -Beck's) (Flax, 1984;Hernández-Urrea and Dario Aristizabal-Ochoa, 2008;Langthjem and Sugiyama, 2000;Ryu et al, 2000;Sugiyama et al, 2000). Beck's generalized load, considered in this paper, is a load for which the direction of the force is determined by the follower coefficient.…”
Section: Introductionmentioning
confidence: 99%
“…A load generated by the simultaneous performance of a conservative (axial) and non-conservative load (follower) was finally introduced to Beck's generalized load with an appropriately calculated follower coefficient (Flax, 1984;Hernández-Urrea and Dario Aristizabal-Ochoa, 2008;Langthjem and Sugiyama, 2000;Ryu et al, 2000;Sugiyama et al, 2000). Sundararajan (1976) and Kounadis (1983) determined the rigidity ranges of a translational, spring supported, non-conservative, slender system, where the system loses stability through flutter and divergence.…”
Section: Introductionmentioning
confidence: 99%