scholarly journals Impact Force Identification of CFRP Laminated Plates Using PZT Piezoelectric Sensors (1st Report, Identification Method and Numerical Simulation)

2004 ◽  
Vol 70 (699) ◽  
pp. 1566-1573 ◽  
Author(s):  
Masanori TAJIMA ◽  
Satoshi MATSUMOTO ◽  
Hisao FUKUNAGA
Author(s):  
Pooya Ghaderi ◽  
Steven I. Rich ◽  
Andrew J. Dick

Indirect impact force identification has attracted researchers due to the simplicity of indirect methods for calculating the applied force during the impact incident. In this paper, an impact force identification method for rod structures is proposed. The proposed method uses the spectral finite element method. The spectral finite element method is a frequency-based finite element method that takes advantage of the benefits of spectral methods and the simplicity of the finite element method. Using the frequency domain method for impact force identification simplifies the calculations and allows for the identification of impact forces with high frequency content, including MHz and above. The impact force identification method uses the collected data of the response of a section of the structure and utilizes the spectral finite element model of the structure to calculate the impact force. The results of the numerical study display strong agreement between the simulated impact force and the identified force. The performance of the force identification method is verified by applying it to experimental data collected from an impacted rod structure.


2012 ◽  
Vol 48 ◽  
pp. 367-374 ◽  
Author(s):  
Vladislav Laš ◽  
Robert Zemčík ◽  
Tomáš Kroupa ◽  
Jan Bartošek

Author(s):  
Xiangying Guo ◽  
Wei Zhang ◽  
Ming-Hui Yao

This paper presents an analysis on the nonlinear dynamics and multi-pulse chaotic motions of a simply-supported symmetric cross-ply composite laminated rectangular thin plate with the parametric and forcing excitations. Firstly, based on the Reddy’s three-order shear deformation plate theory and the model of the von Karman type geometric nonlinearity, the nonlinear governing partial differential equations of motion for the composite laminated rectangular thin plate are derived by using the Hamilton’s principle. Then, using the second-order Galerkin discretization approach, the partial differential governing equations of motion are transformed to nonlinear ordinary differential equations. The case of the primary parametric resonance and 1:1 internal resonance is considered. Four-dimensional averaged equation is obtained by using the method of multiple scales. From the averaged equation obtained here, the theory of normal form is used to give the explicit expressions of normal form. Based on normal form, the energy phase method is utilized to analyze the global bifurcations and multi-pulse chaotic dynamics of the composite laminated rectangular thin plate. The results obtained above illustrate the existence of the chaos for the Smale horseshoe sense in a parametrical and forcing excited composite laminated thin plate. The chaotic motions of the composite laminated rectangular thin plate are also found by using numerical simulation. The results of numerical simulation also indicate that there exist different shapes of the multi-pulse chaotic motions for the composite laminated rectangular thin plate.


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