On the stability of equilibrium of continuous systems Technical report no. 65-1
Stability of equilibrium of linear elastic continuum - Galerkin method
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Stability of equilibrium of linear elastic continuum - Galerkin method
Viscous damping and gyroscopic effects on destabilization in linear system subjected to conservative forces
Sufficiency theorem for stability of linearly viscoelastic solid subjected to partial follower surface tractions
Cantilever bar torsional instability under nonconservative compression loading
Velocity dependent force destabilizing effect in cantilevered continuous pipe conveying fluid at constant velocity
Energy considerations in stability analysis of discrete linear structural systems under nonconservative forces
Models demonstrating instability on nonconservative mechanical systems
Cantilevered continuous pipe conveying fluid at constant velocity, showing that internal and external damping and Coriolis forces may have destabilizing effect
Torsional instability of cantilevered bars, describing effects of distributed nonconservative compressive load at free end
Torsional instability of cantilevered bars, describing effects of distributed nonconservative compressive load at free end
Destabilization of linear system with N degrees of freedom without damping subjected to nonconservative forces
Bending-torsional flutter of uniform swept wing with velocity component aerodynamic-strip theory
Cantilevered continuous pipe conveying fluid at constant velocity, showing that internal and external damping and Coriolis forces may have destabilizing effect
Sufficient condition for stability of linearly viscoelastic continuum subjected to surface tractions following partial deformation of solid are nonconservative and associated with energy source
Adjoint field in elastic stability problems for nondissipative nonconservative systems
Instability modes of cantilevered bars induced by fluid flow through attached pipes, examining cases of torsional and transverse flutter and torsional buckling
Bending torsional flutter of uniform swept wing with velocity component aerodynamic strip theory
Energy method extended to stability analysis of linear system under action of nonconservative forces