Abstract
Stability of a cantilever under an eccentrically applied follower-end-load is considered. It is shown that a bar with warping rigidity may lose stability by bending-torsional flutter, bending-torsional buckling, transverse flutter, or torsional buckling depending on the eccentricity and other parameters. In particular, it is found that the bending-torsional-flutter-load can be considerably reduced when the bar has warping rigidity. The influence of the internal damping forces on the flutter loads is also assessed.
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