Evaluation of Adhesive Bonding Structure in Cryogenic Composite Tank Based on Fracture Mechanics
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- TAKEUCHI Shinsuke
- Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency
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- SATO Eiichi
- Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency
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- ONODA Junjiro
- Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency
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- HIGUCHI Ken
- Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency
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- ARAKAWA Yoji
- Fuji Heavy Industries Ltd.
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抄録
An adhesive bonding structure around a metallic mouthpiece of a cryogenic composite tank was analyzed with fracture mechanics. The energy release rate was formulated analytically by considering difference in strain energies in tension and bending before and after crack growth based on a simplified mathematical model. The analytical results were compared by finite element method calculations for five example tanks; there was a fairly good match between the analytical and numerical results. This analysis provides a guideline for the initial optimal design of a cryogenic composite tank based on fracture mechanics.
収録刊行物
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- TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
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TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES 52 (175), 36-46, 2009
一般社団法人 日本航空宇宙学会
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詳細情報 詳細情報について
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- CRID
- 1390282679055276800
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- NII論文ID
- 10026270223
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- NII書誌ID
- AA0086707X
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- ISSN
- 21894205
- 05493811
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- NDL書誌ID
- 10222437
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- 本文言語コード
- en
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- データソース種別
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- JaLC
- NDL
- Crossref
- CiNii Articles
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- 抄録ライセンスフラグ
- 使用不可