modal characteristics of composite beams with single delamination- a simple analytical technique
Authors
abstract
in the present research, the effects of delamination size and location on vibration characteristics of laminated composite beams are investigated both analytically and numerically. in the analytical method, the delaminated beam is modeled as four interconnected euler–bernoulli beams and the constrained and free mode models are both simulated. the differential stretching and the bending-extension coupling are considered in the formulation. analytical expressions for displacement functions are presented in a simple form based on the basic standard trigonometric and hyperbolic functions. this new technique considerably simplifies the calculations regardless of the number of delaminations. in finite element method, delaminated composite beams are modeled in commercial finite element software, abaqus, and natural frequencies and mode shapes are extracted from the modal analysis. analytical results are compared with finite element ones and available experiments in the literature. finally, the generated database for different sizes and locations of delamination can be used to detect the existence of delamination in laminated composite beams and thento specify the size and location of delamination.
similar resources
Modal Characteristics of Composite Beams with Single Delamination- A Simple Analytical Technique
In the present research, the effects of delamination size and location on vibration characteristics of laminated composite beams are investigated both analytically and numerically. In the analytical method, the delaminated beam is modeled as four interconnected Euler–Bernoulli beams and the constrained and free mode models are both simulated. The differential stretching and the bending-extensio...
full textCompressive Behavior of a Glass/Epoxy Composite Laminates with Single Delamination
The buckling and postbuckling behaviors of a composite beam with single delamination are investigated. A three-dimensional finite element model using the commercial code ANSYS is employed for this purpose. The finite elements analyses have been performed using a linear buckling model based on the solution of the eigenvalues problem, and a non-linear one based on an incremental-iterative method....
full textLocating Delamination in Composite Laminated Beams Using the Zero-Order Mode of Lamb Waves
full text
Static Study of Piezoelectric Bimorph Beams with Delamination Zone
The FOSDT (the First Order Shear Deformation Theory) is taking into consideration to study the static behavior of a bimorph beam, with a delamination zone between the upper and the lower layer. The effect of limit conditions and lengths of the delamination zone are presented in this paper, with a PVDF piezoelectric material application. A FEM “Finite Element Method” is used to discretize the be...
full textExperimental Investigation of the Dynamic Characteristics of Laminated Composite Beams
The laminated composite beams are basic structural components used in a variety of engineering structures such as airplane wings, helicopter blades and turbine blades as well as many others in the aerospace, mechanical, and civil industries. An important element in the dynamic analysis of composite beams is the computation of their natural frequencies and mode shapes. This is important because ...
full textAn Analytical Technique for Solving Nonlinear Oscillators of the Motion of a Rigid Rod Rocking Bock and Tapered Beams
In this paper, a new analytical approach has been presented for solving strongly nonlinear oscillator problems. Iteration perturbation method leads us to high accurate solution. Two different high nonlinear examples are also presented to show the application and accuracy of the presented method. The results are compared with analytical methods and with the numerical solution using Runge-Kutta m...
full textMy Resources
Save resource for easier access later
Journal title:
mechanics of advanced composite structuresPublisher: semnan university
ISSN 2423-4826
volume 1
issue 2 2014
Hosted on Doprax cloud platform doprax.com
copyright © 2015-2023