Nonlinear supersonic flutter of laminated composite plates under thermal loads

1997 ◽  
Vol 65 (5) ◽  
pp. 733-740 ◽  
Author(s):  
D.G. Liaw
1999 ◽  
Author(s):  
Serge Abrate

Abstract In this article, the effect of thermal expansion on laminated composite plates are examined and the influence of the layup is studied using non-dimensional lamination parameters. A maximum of 12 parameters are needed to describe all possible laminates regardless of the number of plies. In some applications, the layup is selected to minimum thermal expansion in a certain direction. We show that thermal expansion cannot be prevented in all directions. Thermal deflections of symmetrically laminated plates that are continuous over many line supports are determined using the Rayleigh-Ritz method. The constitutive equations and the thermal loads are expressed in terms of four non-dimensional lamination parameters. Layups that minimize thermal deflections are determined for several types of composite plates subjected to temperature increases that vary linearly through the thickness.


2019 ◽  
Vol 27 (6) ◽  
pp. 314-322 ◽  
Author(s):  
P Emmanuel Nicholas ◽  
C Dharmaraja ◽  
A Sathya Sofia ◽  
D Vasudevan

Author(s):  
Hasan Kasım

This study aims to determine the ballistic performances of laminated composite plates produced with AA5083-H112 series aluminum and rubber material with high elongation capacity under impact loading. To investigate the effect of rubber compounds, two types of rubber with calendered and damping were prepared. Thanks to the surface treatment applied to the aluminum plates, the rubber–metal adhesion strength was adjusted, and four different laminated composite plate samples were prepared. Calendered rubber was used on the bullet impact surface of all samples, and damping rubber was used on the back. It has been observed that the pressure barrier created by the calendered rubber bullet on the front face provides high performance to absorb energy. A detailed study was carried out on the total thickness of laminated composite plates, the interface adhesion strength between rubber and aluminum layers, and the ballistic performance of aluminum-rubber combinations. It was concluded that the laminated composite plate’s energy absorption would increase, especially by increasing the thickness of the dumping rubber layer on the back of the aluminum sheets. In the strong metal-rubber interface interaction between the rubber and aluminum layer, the bullet is stopped before the pressure barrier is formed. The penetration depth and bulging height increase, and most of the energy are transmitted through the aluminum plate. In the weak metal-rubber interface interaction, a significant portion of the energy is absorbed by the rubber and air thanks to the pressure barrier.


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