FREE VIBRATION ANALYSIS OF STIFFENED LAMINATED COMPOSITE PLATES UNDER AXIAL LOADS
Publish place: 15th Annual Conference of Mechanical Engineering
Publish Year: 1386
نوع سند: مقاله کنفرانسی
زبان: English
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شناسه ملی سند علمی:
ISME15_177
تاریخ نمایه سازی: 8 فروردین 1386
Abstract:
In this study‚ the free bending vibration of orthotropic laminated composite plates with stiffeners subjected to axial loads is carried out using first shear deformation theory and finite element method. Effect of axial tension and compression loads on the natural frequencies of the structure is investigated. Adding stiffeners under the plate increases the natural frequency. The displacements are based on C0 -nine plate bending element and each node has three degree of freedom. Effect of both shear deformation and rotary inertia are implemented in the modeling of plate. The equations of motion are derived using Hamilton's principle. Results indicate the tension loads and stiffeners will increase the natural frequency
while the compression loads reduce the natural frequency. The buckling force of plate is computed by increasing the absolute value of ompressive force until the natural frequency tends to zero. Results of simple cases are compared with finding in literature and good agreements were achieved.
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Authors
Ahmadian
Center of Excellence in design, Robotics and Automation, School of Mechanical Engineering, Sharif University of Technology
Pirbodaghi
Center of Excellence in design Robotics and Automation, School of Mechanical Engineering,Sharif University of Technology
Bonakdar
Center of Excellence in design Robotics and Automation, School of Mechanical Engineering Sharif University of Technology
Moghimizand
Center of Excellence in design Robotics and Automation School of Mechanical Engineering Sharif University of Technology
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