Divergence and flutter instability of elastically restrained structures under follower forces

DOI10.1016/0020-7225(81)90089-6zbMath0446.73047OpenAlexW1973386441MaRDI QIDQ1146036

Anthony N. Kounadis

Publication date: 1981

Published in: International Journal of Engineering Science (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/0020-7225(81)90089-6

zbMATH Keywords

instabilitycritical loadcompressive follower forcesdivergence or flutter type instabilitydivergence type non-conservatively loadedelastically restrained simple structures

Mathematics Subject Classification ID

Vibrations in dynamical problems in solid mechanics (74H45) Fluid-solid interactions (including aero- and hydro-elasticity, porosity, etc.) (74F10) Stability of dynamical problems in solid mechanics (74H55)

Related Items (9)

Divergence of a rotating shaft with an intermediate support and conservative axial loads ⋮ Flutter of a cantilever rod with a relocatable lumped mass ⋮ Damping effects on the dynamic stability of a rod subjected to intermediate follower loads ⋮ The regions of flutter and divergence instability of a column subjected to Beck's generalized load, taking into account the torsional flexibility of the loaded end of the column ⋮ Flutter and vibration of elastically restrained nanowires under a nonconservative force ⋮ THE STABILITY AND FREE VIBRATIONS OF A COLUMN SUBJECTED TO A CONSERVATIVE LOAD GENERATED BY A HEAD WITH A PARABOLIC CONTOUR ⋮ Flutter instability of damped plates under combined conservative and nonconservative loads ⋮ Divergence and flutter of nonconservative systems with intermediate support ⋮ Flutter loads of a Timoshenko beam-column under a follower force governed by two variants of equations of motion

Cites Work

• On a lower bound theorem for the buckling load of elastic beams subjected to nonconservative, compressive follower loads
• Application of the Galerkin and Ritz methods to nonconservative problems of elastic stability
• Divergence Buckling of a Simple Frame, Subject to a Follower Force

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