Honeycomb structures manufactured by a new method and its failure analysis

Lijun Wang, Kazuya Saito

研究成果: Contribution to journalConference article査読

抄録

Nowadays, honeycomb sandwich panle is widely used in the field of aircraft and spacecraft, due to its light weight, high strength and good impact resistance. So the stability and buckling behavior of the structure are crucially important. In the present work, two type aluminum honeycomb sandwich panles were manufactured by a new manufacturing method (i.e. a press and folding process). To evaluate the structural failure of the panle, the three-point bending test was carried out, and found that the face sheets and the honeycomb core were splited open under a local load, but the panle has not been completely failure. In addition, the buckling behavior of the panle was implemented with finite element analysis (FEA).

本文言語英語
論文番号012003
ジャーナルJournal of Physics: Conference Series
1733
1
DOI
出版ステータス出版済み - 1 19 2021
イベント2nd International Conference on Trends in Mechanical and Aerospace, TMAE 2020 - Washington, Virtual, 米国
継続期間: 9 25 20209 27 2020

All Science Journal Classification (ASJC) codes

  • 物理学および天文学(全般)

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