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Experimental and Modeling Study of Open-Hole Composite Laminates Under Tension Read chapter Read first chapter

2023 | OriginalPaper | Chapter

Simulation and Test Study on Composite Honeycomb Sandwich Panel

Authors : Yang Kun, Yan Qun, Xu Fei

Published in: Proceedings of the 10th Chinese Society of Aeronautics and Astronautics Youth Forum

Publisher: Springer Nature Singapore

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Abstract

Composite honeycomb sandwich panel is one of the ideal and most efficient structural forms for aircraft structures. In this paper, a finite element analysis model of honeycomb sandwich structure is established. Firstly, the natural vibration mode and frequency of the model are calculated and compared with the test results. In order to verify the calculated acceleration and strain results, a response test of the honeycomb sandwich structure under vibration is further carried out. The simulation of the model is in good agreement with the experimental results, which verifies the effectiveness and accuracy of the proposed analysis and method.

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Metadata
Title
Simulation and Test Study on Composite Honeycomb Sandwich Panel
Authors
Yang Kun
Yan Qun
Xu Fei
Copyright Year
2023
Publisher
Springer Nature Singapore
Book
Proceedings of the 10th Chinese Society of Aeronautics and Astronautics Youth Forum

Print ISBN: 978-981-19-7651-3

Electronic ISBN: 978-981-19-7652-0

Copyright Year: 2023

DOI
https://doi.org/10.1007/978-981-19-7652-0_34

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