Buckling and Vibration Behavior of Composite Beam due to Axially Varying In-plane Loads

In this work buckling and vibration behavior of composite beam is analyzed based on the shear and normal deformable beam theory (SNDBT) by using Ritz method. The effects of aspect ratios, boundary conditions, fiber angles on the buckling and vibration subjected to non-uniform axial loads studied in...

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Bibliographic Details
Published in:IOP conference series. Materials Science and Engineering 2021-04, Vol.1128 (1), p.12043
Main Authors: Kanade, Sangram Anil, Chinnapandi, Lenin Babu Mailan, Jeyaraj, P, Subramanian, Jeyanthi
Format: Article
Language:English
Subjects:
Aspect ratio
Axial loads
Boundary conditions
Buckling
Composite beams
Deformation effects
Dimensionless numbers
Formability
Noise control
Resonant frequencies
Ritz method
Vibration analysis
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Summary:In this work buckling and vibration behavior of composite beam is analyzed based on the shear and normal deformable beam theory (SNDBT) by using Ritz method. The effects of aspect ratios, boundary conditions, fiber angles on the buckling and vibration subjected to non-uniform axial loads studied in detail. The obtained numerical results in terms of dimensionless fundamental frequencies and dimensionless first critical buckling loads are compared with the results from previous research for convergence studies.
ISSN:1757-8981
1757-899X
DOI:10.1088/1757-899X/1128/1/012043