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Exact(52)
Hence, linearized model of ball and Beam is considered.
The linear dynamics of a two-layer beam is considered.
A cross-ply laminated composite beam is considered as well.
Sinusoidal base excitation of the AFM cantilevered beam is considered.
A truncated beam is considered as part of a hypothetical complete beam.
When the beam is considered rigid, the two-degree-of-freedom model is employed.
Similar(8)
Transverse vibrations of an axially moving beam are considered.
To validate the analytical approach, experimental results for a simply supported beam are considered.
Laminated composite plate and beam are considered as simple morphing structural components.
Both the axial and rotary inertia of the beam are considered in the present analysis.
Elastic flexural waves in an unloaded and unsupported segment of a non-uniform beam were considered.
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