A stress recovery procedure for laminated composite plates based on strong-form equilibrium enforced via the RBF Kansa method

2020 ◽  
Vol 244 ◽  
pp. 112292
Author(s):  
Andrea Chiappa ◽  
Corrado Groth ◽  
Alessandro Reali ◽  
Marco Evangelos Biancolini
Keyword(s):  
Laminated Composite ◽  
Composite Plates ◽  
Strong Form ◽  
Stress Recovery ◽  
Laminated Composite Plates ◽  
Kansa Method ◽  
Recovery Procedure

scholarly journals Fast and accurate elastic analysis of laminated composite plates via isogeometric collocation and an equilibrium-based stress recovery approach

2019 ◽  
Vol 225 ◽  
pp. 111026 ◽  
Author(s):  
Alessia Patton ◽  
John-Eric Dufour ◽  
Pablo Antolin ◽  
Alessandro Reali
Keyword(s):  
Laminated Composite ◽  
Composite Plates ◽  
Stress Recovery ◽  
Elastic Analysis ◽  
Laminated Composite Plates ◽  
Recovery Approach

Stability and accuracy of three Fourier expansion-based strong form finite elements for the free vibration analysis of laminated composite plates

2017 ◽  
Vol 111 (4) ◽  
pp. 354-382 ◽  
Author(s):  
Nicholas Fantuzzi ◽  
Francesco Tornabene ◽  
Michele Bacciocchi ◽  
Ana M. A. Neves ◽  
Antonio J. M. Ferreira
Keyword(s):  
Finite Elements ◽  
Free Vibration ◽  
Vibration Analysis ◽  
Fourier Expansion ◽  
Laminated Composite ◽  
Free Vibration Analysis ◽  
Composite Plates ◽  
Strong Form ◽  
Laminated Composite Plates ◽  
Stability And Accuracy

Ballistic performance of composite structure configurations with high elongation calendered rubber layer laminated to AA5083-H112 aluminum alloy

2021 ◽  
pp. 146442072110145
Author(s):  
Hasan Kasım
Keyword(s):  
Adhesion Strength ◽  
Laminated Composite ◽  
Composite Plates ◽  
Front Face ◽  
Laminated Composite Plates ◽  
Ballistic Performance ◽  
Rubber Layer ◽  
Interface Interaction ◽  
Metal Rubber ◽  
High Elongation

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.

Sign in / Sign up

Export Citation Format

Share Document