Free vibration analysis of polymer pin-reinforced foam core sandwich composite panels

Author:

Shishir Md Asif Rezwan12,Zhang Zhaoyuan3,Cai Deng’an1ORCID,Wang Xinwei1,Xu Qinghua1

Affiliation:

1. State Key Laboratory of Mechanics and Control of Mechanical Structures, Nanjing University of Aeronautics and Astronautics, Nanjing, China

2. College of International Education, Nanjing University of Aeronautics and Astronautics, Nanjing, China

3. College of Mechanical and Electrical Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing, China

Abstract

This study deals with numerical and experimental free vibration analysis of through-the-thickness cylindrical polymer pin-reinforced foam core sandwich composite panels of two different core thicknesses. Four different pin-reinforcement configurations with varying pin diameters and pin center distances were used. First five non-zero eigenfrequencies were retrieved along with their eigenmodes in the numerical analysis. Experimental modal analysis was done for the validation of the numerical analysis. The results revealed that the pin-configuration with the densest pin allocation and the biggest pin diameter provided the highest natural frequencies, and the non-reinforced composites had the lowest natural frequencies. The increase in the pin diameter had a slightly more pronounced effect on the increase of the eigenfrequencies than the increase in the pin’s densities. This work also demonstrated the impact of the core thickness on the natural frequencies.

Funder

Natural Science Foundation of Jiangsu Province

National Natural Science Foundation of China

National Key Basic Research and Development Program

Publisher

SAGE Publications

Subject

Materials Chemistry,Polymers and Plastics,Mechanical Engineering,Mechanics of Materials,Ceramics and Composites

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