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Fatigue of Aircraft Structures
AHEAD OF PRINT
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Effect of Thermal and External Load on Mechanical Behaviour on CFRP/Aluminium Hybrid Joints
Takao Okada
Takao Okada
Japan Aerospace Exploration Agency
Chofu-shi, Japan
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Okada, Takao
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Tomo Takeda
Tomo Takeda
Japan Aerospace Exploration Agency
Chofu-shi, Japan
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Takeda, Tomo
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Hisashi Kumazawa
Hisashi Kumazawa
Japan Aerospace Exploration Agency
Chofu-shi, Japan
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Kumazawa, Hisashi
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Toshiyuki Kasahara
Toshiyuki Kasahara
Adecco Group Japan
Chiyoda-ku, Japan
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Kasahara, Toshiyuki
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Sho Miyashita
Sho Miyashita
Former Japan Aerospace Exploration Agency
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Miyashita, Sho
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Koichi Yamada
Koichi Yamada
Former Japan Aerospace Exploration Agency
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Yamada, Koichi
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Kasumi Nagao
Kasumi Nagao
Former Japan Aerospace Exploration Agency
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Nagao, Kasumi
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Yuichiro Aoki
Yuichiro Aoki
Former Japan Aerospace Exploration Agency
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Aoki, Yuichiro
Jul 07, 2025
Fatigue of Aircraft Structures
AHEAD OF PRINT
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Article Category:
Research Article
Published Online:
Jul 07, 2025
DOI:
https://doi.org/10.2478/fas-2024-0002
Keywords
Hybrid joints
,
Thermal and external load
,
Hysteresis loop
,
Fatigue fracture
,
Finite element analysis
© 2025 Takao Okada et al., published by Sciendo
This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 3.0 License.