Acoustic Fatigue Research for Honeycomb Sandwich Structure with Impact Damage Based on Vibro-Acoustic Coupling Analysis

Author(s):  
Ruowei Li ◽  
Haitao Zhao ◽  
Mingqing Yuan ◽  
Ji’an Chen
2009 ◽  
Vol 79-82 ◽  
pp. 1727-1730 ◽  
Author(s):  
Xiao Dong He ◽  
Xiang Hao Kong ◽  
Li Ping Shi ◽  
Ming Wei Li

ARMOR TPS panel is above the whole ARMOR TPS, and the metal honeycomb sandwich structure is the surface of the ARMOR TPS panel. So the metal honeycomb sandwich structure plays an important role in the ARMOR TPS, while it bears the flight dynamic pressure and stands against the flight dynamic calefaction. So the active environment of metal honeycomb sandwich structure is very formidable. We have to discuss any extreme situation, for reason of making sure aerial vehicle is safe. And high-frequency vibration is one of active environment. In this paper we have analyzed high-frequency vibration response of metal honeycomb sandwich structure. We processed high-frequency vibration experiment by simulating true aerial environment. Sequentially we operated high-frequency vibration experiment of metal honeycomb sandwich structure with cracks, notches and holes. Then finite-element analysis was performed by way of validating the experiment results. Haynes214 is a good high temperature alloy material of both face sheet and core at present, so we choose it in this paper.


2017 ◽  
Vol 81 ◽  
pp. 69-78 ◽  
Author(s):  
Hanxue Zhao ◽  
Zhenggan Zhou ◽  
Jin Fan ◽  
Gen Li ◽  
Guangkai Sun

2010 ◽  
pp. 223-235

Abstract The honeycomb sandwich structure composite is a very efficient and complex structure widely used in the aircraft industry. Honeycomb-cored sandwich panels increase part stiffness at a lower weight than monolithic composite materials. This chapter describes the analysis of the intermingling of the film adhesive/prepreg resin system. It discusses the causes and effects of honeycomb core movement, which results in core crush. The chapter also explains the formation of a void in honeycomb composites and the failure mechanisms in honeycomb sandwich structure composites.


AIP Advances ◽  
2020 ◽  
Vol 10 (2) ◽  
pp. 025201 ◽  
Author(s):  
Jiawei Wang ◽  
Bin Li ◽  
Yongxiang Zhu ◽  
Weiping Liu ◽  
Lixiong Wu ◽  
...  

2020 ◽  
Vol 146 ◽  
pp. 106489 ◽  
Author(s):  
Ruixiang Bai ◽  
Hongqi Ou ◽  
Kewang Peng ◽  
Wen Wu ◽  
Zhenkun Lei ◽  
...  

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