scholarly journals Natural Frequencies Of Internally-Doubly-Tapered Laminated Composite Beams

Author(s):  
Amin Fazili ◽  
Rajamohan Ganesan
2018 ◽  
Vol 18 (11) ◽  
pp. 1850130 ◽  
Author(s):  
Ngoc-Duong Nguyen ◽  
Trung-Kien Nguyen ◽  
Thuc P. Vo ◽  
Huu-Tai Thai

In this paper, the Ritz-based solutions are developed for the bending, buckling and vibration behaviors of laminated composite beams with arbitrary lay-ups. A quasi-3D theory, which accounts for a higher-order variation of both the axial and transverse displacements, is used to capture the effects of both shear and normal deformations on the behaviors of composite beams. Numerical results for various boundary conditions are presented and compared with existing ones available in the literature. Besides, the effects of fiber angle, span-to-height ratio, material anisotropy and Poisson’s ratio on the displacements, stresses, natural frequencies and buckling loads of the composite beams are investigated.


2021 ◽  
Vol 29 (9_suppl) ◽  
pp. S1371-S1385
Author(s):  
Priyadarshi Das ◽  
Shishir K Sahu

The free vibration study of industry-driven woven fibre laminated carbon/epoxy composite beam is addressed through experimental and numerical modal analysis in the present research work. The experimental modal analysis is performed using the vibration Fast Fourier Transform (FFT) analyser and the natural frequencies are realized in the PULSE environment. A linear beam model is simulated in ABAQUS finite element (FE) software, adopting a solid deformable 8-nodded element with five degrees of freedom (DOF) per node from the ABAQUS library for numerical computation of natural frequencies. A satisfactory agreement is achieved between the experimental and numerical results. The effects of ply-orientation, number of plies, lamination scheme and aspect ratios with different boundary conditions on the natural frequencies are studied. The results confirmed that the predicted vibration characteristics of laminated composite beams are sensitive to the adopted parameters for the investigation. The present study will help to understand the dynamic behaviour for laminated composite beams and serve as an experimental benchmark result within the frequency domain.


2015 ◽  
Vol 61 (2) ◽  
pp. 161-178 ◽  
Author(s):  
G. Abdollahzadeh ◽  
M. Ahmadi

AbstractIn this stud y, we attempt to analyse free nonlinear vibrations of buckling in laminated composite beams. Two new methods are applied to obtain the analytical solution of the nonlinear governing equation of the problem. The effects of different parameters on the ratio of nonlinear to linear natural frequencies of the beams are studied. These methods give us an agreement with numerical results for the whole range of the oscillation amplitude.


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