{"created":"2023-06-20T14:39:00.353300+00:00","id":5669,"links":{},"metadata":{"_buckets":{"deposit":"be67183d-98c3-4ca0-8684-e67366b1a571"},"_deposit":{"created_by":1,"id":"5669","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"5669"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00005669","sets":["1887:1891","9:789:972:991"]},"author_link":["27786","27785","27784","27783","27787","27782"],"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2008-02-29","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"149","bibliographicPageStart":"142","bibliographicVolumeNumber":"JAXA-SP-07-008E","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構特別資料"},{"bibliographic_title":"JAXA Special Publication: Proceedings of Lectures and Workshop International: Recent Advances in Multidisciplinary Technology and Modeling","bibliographic_titleLang":"en"}]}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"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.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0063824014","subitem_description_type":"Other"}]},"item_5_description_33":{"attribute_name":"レポート番号","attribute_value_mlt":[{"subitem_description":"レポート番号: JAXA-SP-07-008E","subitem_description_type":"Other"}]},"item_5_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙航空研究開発機構"}]},"item_5_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Japan Aerospace Exploration Agency (JAXA)"}]},"item_5_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"1349-113X","subitem_source_identifier_type":"ISSN"}]},"item_5_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AA11984031","subitem_source_identifier_type":"NCID"}]},"item_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"九州大学 大学院工学府"},{"subitem_text_value":"九州大学 大学院工学府"},{"subitem_text_value":"九州大学 大学院工学府"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Kyushu University Graduate School of Engineering"},{"subitem_text_language":"en","subitem_text_value":"Kyushu University Graduate School of Engineering"},{"subitem_text_language":"en","subitem_text_value":"Kyushu University Graduate School of Engineering"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"朝野, 裕樹"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"仮屋崎, 剛大"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"室園, 昌彦"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Asano, Yuki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kariyazaki, Takehiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Murozono, Masahiko","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_files":{"attribute_name":"ファイル情報","attribute_type":"file","attribute_value_mlt":[{"accessrole":"open_date","date":[{"dateType":"Available","dateValue":"2020-01-16"}],"displaytype":"detail","filename":"63824014.pdf","filesize":[{"value":"1.2 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"63824014.pdf","url":"https://jaxa.repo.nii.ac.jp/record/5669/files/63824014.pdf"},"version_id":"3ed377a0-5bc2-4d19-818f-d921cdf4a14c"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"熱変形","subitem_subject_scheme":"Other"},{"subitem_subject":"積層ビーム","subitem_subject_scheme":"Other"},{"subitem_subject":"熱応力","subitem_subject_scheme":"Other"},{"subitem_subject":"複合材料","subitem_subject_scheme":"Other"},{"subitem_subject":"温度分布","subitem_subject_scheme":"Other"},{"subitem_subject":"層間応力","subitem_subject_scheme":"Other"},{"subitem_subject":"熱膨張","subitem_subject_scheme":"Other"},{"subitem_subject":"弾性係数","subitem_subject_scheme":"Other"},{"subitem_subject":"熱伝導度","subitem_subject_scheme":"Other"},{"subitem_subject":"宇宙機構造材料","subitem_subject_scheme":"Other"},{"subitem_subject":"航空宇宙環境","subitem_subject_scheme":"Other"},{"subitem_subject":"thermal deformation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"laminated beam","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"thermal stress","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"composite material","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"temperature distribution","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"interlaminar stress","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"thermal expansion","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"modulus of elasticity","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"thermal conductivity","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"spacecraft construction material","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerospace environment","subitem_subject_language":"en","subitem_subject_scheme":"Other"}]},"item_language":{"attribute_name":"言語","attribute_value_mlt":[{"subitem_language":"eng"}]},"item_resource_type":{"attribute_name":"資源タイプ","attribute_value_mlt":[{"resourcetype":"conference paper","resourceuri":"http://purl.org/coar/resource_type/c_5794"}]},"item_title":"Minimization of unsteady thermal deformation by using laminated structures under the stress restrictions","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Minimization of unsteady thermal deformation by using laminated structures under the stress restrictions","subitem_title_language":"en"}]},"item_type_id":"5","owner":"1","path":["991","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"5669","relation_version_is_last":true,"title":["Minimization of unsteady thermal deformation by using laminated structures under the stress restrictions"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T08:09:38.891381+00:00"}