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Minimization of unsteady thermal deformation by using laminated structures under the stress restrictions
https://jaxa.repo.nii.ac.jp/records/5669
https://jaxa.repo.nii.ac.jp/records/5669ca94067f-0698-4eb8-9c0a-d306c18fc001
名前 / ファイル | ライセンス | アクション |
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63824014.pdf (1.2 MB)
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Item type | 会議発表論文 / Conference Paper(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
言語 | en | |||||
タイトル | Minimization of unsteady thermal deformation by using laminated structures under the stress restrictions | |||||
言語 | ||||||
言語 | eng | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 熱変形 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 積層ビーム | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 熱応力 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 複合材料 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 温度分布 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 層間応力 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 熱膨張 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 弾性係数 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 熱伝導度 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 宇宙機構造材料 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 航空宇宙環境 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | thermal deformation | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | laminated beam | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | thermal stress | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | composite material | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | temperature distribution | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | interlaminar stress | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | thermal expansion | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | modulus of elasticity | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | thermal conductivity | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | spacecraft construction material | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | aerospace environment | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_5794 | |||||
資源タイプ | conference paper | |||||
著者 |
朝野, 裕樹
× 朝野, 裕樹× 仮屋崎, 剛大× 室園, 昌彦× Asano, Yuki× Kariyazaki, Takehiro× Murozono, Masahiko |
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著者所属 | ||||||
九州大学 大学院工学府 | ||||||
著者所属 | ||||||
九州大学 大学院工学府 | ||||||
著者所属 | ||||||
九州大学 大学院工学府 | ||||||
著者所属(英) | ||||||
en | ||||||
Kyushu University Graduate School of Engineering | ||||||
著者所属(英) | ||||||
en | ||||||
Kyushu University Graduate School of Engineering | ||||||
著者所属(英) | ||||||
en | ||||||
Kyushu University Graduate School of Engineering | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構 | |||||
出版者(英) | ||||||
出版者 | Japan Aerospace Exploration Agency (JAXA) | |||||
書誌情報 |
宇宙航空研究開発機構特別資料 en : JAXA Special Publication: Proceedings of Lectures and Workshop International: Recent Advances in Multidisciplinary Technology and Modeling 巻 JAXA-SP-07-008E, p. 142-149, 発行日 2008-02-29 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Laminated beam structures are designed in order to minimize thermal deformations in steady or unsteady temperature field. To suppress thermal deformation, composite materials that has negative longitudinal coefficient of thermal expansion are layered with material that has positive Coefficient of Thermal Expansion (CTE). Assuming steady temperature fields, beam with no strain at central axis and no curvature can be designed. In unsteady temperature fields, it is possible to suppress thermal deformations while lowering thermal stresses. If it takes a long time until the temperature distribution get steady, the beam should be designed with considering unsteady temperature distributions because the beam that was designed with considering only steady temperature distribution could have large thermal deformations in its transitional period. For suppressing thermal deformations, interlaminar shearing stress, and interlaminar moment, materials with large Young's Modulus, CTE, and thermal conductivity are effective to use for low temperature side, oppositely, materials with small Young's Modulus, CTE, and thermal conductivity are effective to use for high temperature side. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 1349-113X | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA11984031 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0063824014 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: JAXA-SP-07-008E |