Dynamic response of Nomex honeycomb sandwich panels subjected to aluminum foam projectile <scp>impact–An</scp> experimental study-Reference-Cited by-同舟云学术

Dynamic response of Nomex honeycomb sandwich panels subjected to aluminum foam projectile impact–An experimental study

Published:2022-11-14 Issue:2 Volume:44 Page:1017-1037
ISSN:0272-8397
Container-title:Polymer Composites
language:en
Short-container-title:Polymer Composites

Author:

Deng Yunfei¹,Hu Xiaoyu²^ORCID,Yang Xiaoyue²,Huang Ziqiang²,Wang Yuetong²^ORCID,Zhou Chunping³

Affiliation:

1. Key Laboratory of Civil Aviation Aircraft Airworthiness Certification Technology Civil Aviation University of China Tianjin People's Republic of China

2. College of Aeronautical Engineer Civil Aviation University of China Tianjin China

3. Aeronautical Science Key Lab for High Performance Electromagnetic Windows AVIC Research Institute For Special Structures of Aeronautical Composite Jinan People's Republic of China

Publisher

Wiley

Subject

Materials Chemistry,Polymers and Plastics,General Chemistry,Ceramics and Composites

Link

https://onlinelibrary.wiley.com/doi/pdf/10.1002/pc.27151

Reference39 articles.

1. Experimental and numerical analysis of dynamic compressive response of Nomex honeycombs

2. Bioinspired engineering of honeycomb structure – Using nature to inspire human innovation

3. Mechanical properties of Nomex honeycomb sandwich panels under dynamic impact

4. State‐of‐the‐art review on honeycomb sandwich composite structures with an emphasis on filler materials

5. Numerical analysis of face sheet buckling for a CFRP/Nomex honeycomb sandwich panel subjected to bending loading

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