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Effect of Thermal and External Load on Mechanical Behaviour on CFRP/Aluminium Hybrid Joints Cover

Effect of Thermal and External Load on Mechanical Behaviour on CFRP/Aluminium Hybrid Joints

Fatigue of Aircraft Structures
Volume 2024 (2024): Issue 16 (December 2024)
By: Takao Okada,  Tomo Takeda,  Hisashi Kumazawa,  Toshiyuki Kasahara,  Sho Miyashita,  Koichi Yamada,  Kasumi Nagao and  Yuichiro Aoki  
Open Access
|Jul 2025

Authors

Takao Okada

okada.takao@jaxa.jp

Japan Aerospace Exploration Agency, Chofu-shi, Japan

Tomo Takeda

Japan Aerospace Exploration Agency, Chofu-shi, Japan

Hisashi Kumazawa

Japan Aerospace Exploration Agency, Chofu-shi, Japan

Toshiyuki Kasahara

Adecco Group Japan, Chiyoda-ku, Japan

Sho Miyashita

Former Japan Aerospace Exploration Agency

Koichi Yamada

Former Japan Aerospace Exploration Agency

Kasumi Nagao

Former Japan Aerospace Exploration Agency

Yuichiro Aoki

Former Japan Aerospace Exploration Agency
DOI: https://doi.org/10.2478/fas-2024-0002 | Journal eISSN: 2300-7591 | Journal ISSN: 2081-7738
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Language: English
Page range: 16 - 28
Published on: Jul 7, 2025
Published by: ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
In partnership with: Paradigm Publishing Services
Publication frequency: 1 issue per year
Keywords:
Hybrid joints,
Thermal and external load,
Hysteresis loop,
Fatigue fracture,
Finite element analysis
Related subjects:
Engineering,
Introductions and overviews,
Engineering, other

© 2025 Takao Okada, Tomo Takeda, Hisashi Kumazawa, Toshiyuki Kasahara, Sho Miyashita, Koichi Yamada, Kasumi Nagao, Yuichiro Aoki, published by ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 3.0 License.

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