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DYNAMIC RESPONSE OF NON-UNIFORM COMPOSITE BEAMS

โœ Scribed by S. Ramalingeswara Rao; N. Ganesan


Publisher
Elsevier Science
Year
1997
Tongue
English
Weight
605 KB
Volume
200
Category
Article
ISSN
0022-460X

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โœฆ Synopsis


The harmonic response of tapered composite beams is investigated by using a finite element model. Only uniaxial bending is considered. The Poisson effect is incorporated in the formulation of the beam constitutive equations. Interlaminar stresses are evaluated by using stress equilibrium equations. The effects of in-plane inertia and rotary inertia are also considered in the formulation of the mass matrix. A parametric study is carried out to investigate the influence of taper profile and taper parameter. Linearly varying thickness variations of increasing, decreasing, decreasing-increasing and increasing-decreasing types are considered.


๐Ÿ“œ SIMILAR VOLUMES


DYNAMIC RESPONSE OF TAPERED COMPOSITE BE
โœ S. Ramalingerswara Rao; N. Ganesan ๐Ÿ“‚ Article ๐Ÿ“… 1995 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 600 KB

Harmonic response of tapered composite beams is investiaged by using a finite element model based on a higher order shear deformation theory. Only uniaxial bending is considered and the interlaminar shear stresses are neglected. The Poisson ratio effect is incorporated in the formulation of beam con