Non-linear normal modes and the associated frequencies of a uniform beam with simply-supported or clamped conditions at both ends have been derived. Some restricted orthogonality conditions have been pointed out. The effects of the longitudinal inertia on the non-linear transverse motion are shown t
ANALYSIS OF NON-LINEAR PIEZOTHERMOELASTIC LAMINATED BEAMS WITH ELECTRIC AND TEMPERATURE EFFECTS
โ Scribed by Y. Bao; H.S. Tzou; V.B. Venkayya
- Publisher
- Elsevier Science
- Year
- 1998
- Tongue
- English
- Weight
- 228 KB
- Volume
- 209
- Category
- Article
- ISSN
- 0022-460X
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โฆ Synopsis
Conventional analyses of piezoelectric laminated structures are based on linear theories. Investigations of non-linear characteristics are still relatively scarce. In this paper, static, dynamic, and control effects of a piezothermoelastic laminated beam with an initial non-linear large static deflection (the von Karman type geometric non-linear deformation) and temperature and electric inputs are studied. It is assumed that the piezoelectric layers are uniformly distributed on the top and bottom surfaces of the beam. Beam equations incorporating the non-linear deflections, piezoelectric layers, temperature and electric effects are simplified from the generic piezothermoelastic shell equations. Analytical solutions of non-linear static deflection and eigenvalue problems of the non-linearly deformed beam including temperature and electric effects are derived. Active control effects on non-linear static deflections and natural frequencies imposed by the piezoelectric actuators via high control voltages are investigated. A numerical example is provided and response behavior is investigated.
๐ SIMILAR VOLUMES
The relation between the wave propagation and the free vibration in a travelling beam with simple supports has been thoroughly investigated. The frequency equation of such a beam has been derived using the phase-closure principle. Since the characters of the waves change drastically as the axial spe
The wave propagation in a simply supported travelling beam, studied in Part I of this paper, has been used to derive the forced responses. Based upon the wave-propagation principles, a simple method for constructing the closed-form transfer function of such a beam has been presented. The use of this