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摘要:
A low velocity impact response study has been carried out on glass fibre composite laminates, made up of regular aircraft grade epoxy (GFRP) and shape memory polymer (GF-SMP). Under various impact loading intensities (4J, 6J, 12J), the responses are measured by a network of PZT (Lead Zirconate Titanate) sensors. A signal analysis methodology is subsequently developed to process the very high frequency (60 MHz) sampled data. In two frequency bands, namely 0 - 2000 Hz and 0 - 100 KHz, the results are examined and the transient dynamic behaviours of the composite laminates are evaluated. It is observed that both the laminates have generated the high frequency structural waves (0 - 100 KHz), which can be exploited to examine the BVID. However, GF-SMP laminate has shown some advantage in terms of energy dissipation in the structural frequency band (<2000 Hz). Further, the GF-SMP laminate has demonstrated its capability to generate very high frequency structural waves, which could carry the damage information like BVID due to impact event to nearby sensors for impact event monitoring and health assessment.
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篇名 Low Velocity Impact Response on GFRP and GF-SMP Panels in Structural and High Frequency Bands
来源期刊 航空科学与技术(英文) 学科 工学
关键词 Impact Low Velocity PZT Patches GFRP Composite Laminate Transient Dynamics
年,卷(期) 2020,(2) 所属期刊栏目
研究方向 页码范围 58-70
页数 13页 分类号 TB3
字数 语种
DOI
五维指标
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研究主题发展历程
节点文献
Impact
Low
Velocity
PZT
Patches
GFRP
Composite
Laminate
Transient
Dynamics
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研究分支
研究去脉
引文网络交叉学科
相关学者/机构
期刊影响力
航空科学与技术(英文)
季刊
2473-6708
武汉市江夏区汤逊湖北路38号光谷总部空间
出版文献量(篇)
23
总下载数(次)
0
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