WEKO3
アイテム
{"_buckets": {"deposit": "1fe6d66e-e9e8-4977-b9e2-b8c868377a63"}, "_deposit": {"created_by": 1, "id": "32514", "owners": [1], "pid": {"revision_id": 0, "type": "depid", "value": "32514"}, "status": "published"}, "_oai": {"id": "oai:jaxa.repo.nii.ac.jp:00032514", "sets": ["1890", "1910"]}, "author_link": ["409642", "409639", "409640", "409641", "409635", "409637", "409636", "409638"], "item_9_alternative_title_2": {"attribute_name": "その他のタイトル(英)", "attribute_value_mlt": [{"subitem_alternative_title": "Minimum Weight Design of Stiffened Cylindrical Shells under Pure Bending"}]}, "item_9_biblio_info_10": {"attribute_name": "書誌情報", "attribute_value_mlt": [{"bibliographicIssueDates": {"bibliographicIssueDate": "1979-11", "bibliographicIssueDateType": "Issued"}, "bibliographicIssueNumber": "4", "bibliographicPageEnd": "878", "bibliographicPageStart": "865", "bibliographicVolumeNumber": "15", "bibliographic_titles": [{"bibliographic_title": "東京大学宇宙航空研究所報告"}]}]}, "item_9_description_16": {"attribute_name": "抄録", "attribute_value_mlt": [{"subitem_description": "曲げモーメント75 ton-mを受けるフレーム(円きょう)と縦通材で補強された直径2,440 mmの円筒殼の最小重量設計を行い,設計の妥当性を縮尺比1/3のモデルによる実験により確認した.", "subitem_description_type": "Abstract"}]}, "item_9_description_17": {"attribute_name": "抄録(英)", "attribute_value_mlt": [{"subitem_description": "A method of structural optimization is applied in designing circular cylindrical shells under bending. The cylindrical shells are stiffened both longitudinally and circumferentially. A one-third scale model of the designed cylindrical shell has been made and tested to check the validity of the design.", "subitem_description_type": "Other"}]}, "item_9_description_32": {"attribute_name": "資料番号", "attribute_value_mlt": [{"subitem_description": "資料番号: SA0125803000", "subitem_description_type": "Other"}]}, "item_9_publisher_8": {"attribute_name": "出版者", "attribute_value_mlt": [{"subitem_publisher": "東京大学宇宙航空研究所"}]}, "item_9_source_id_21": {"attribute_name": "ISSN", "attribute_value_mlt": [{"subitem_source_identifier": "0563-8100", "subitem_source_identifier_type": "ISSN"}]}, "item_9_source_id_24": {"attribute_name": "書誌レコードID", "attribute_value_mlt": [{"subitem_source_identifier": "AN00161914", "subitem_source_identifier_type": "NCID"}]}, "item_9_text_34": {"attribute_name": "メタデータ提供者", "attribute_value_mlt": [{"subitem_text_value": "メタデータ提供者: ISASNII"}]}, "item_9_text_35": {"attribute_name": "JAXAカテゴリ", "attribute_value_mlt": [{"subitem_text_value": "JAXAカテゴリ: 宇宙科学研究所"}]}, "item_9_text_43": {"attribute_name": "DSpaceコレクション番号", "attribute_value_mlt": [{"subitem_text_value": "DSpaceコレクション番号: 6"}]}, "item_9_text_6": {"attribute_name": "著者所属", "attribute_value_mlt": [{"subitem_text_value": "東京大学宇宙航空研究所"}, {"subitem_text_value": "東京大学宇宙航空研究所"}, {"subitem_text_value": "東京大学宇宙航空研究所"}, {"subitem_text_value": "東京大学宇宙航空研究所"}]}, "item_9_text_7": {"attribute_name": "著者所属(英)", "attribute_value_mlt": [{"subitem_text_language": "en", "subitem_text_value": "Institute of Space and Aeronautical Science, University of Tokyo"}, {"subitem_text_language": "en", "subitem_text_value": "Institute of Space and Aeronautical Science, University of Tokyo"}, {"subitem_text_language": "en", "subitem_text_value": "Institute of Space and Aeronautical Science, University of Tokyo"}, {"subitem_text_language": "en", "subitem_text_value": "Institute of Space and Aeronautical Science, University of Tokyo"}]}, "item_creator": {"attribute_name": "著者", "attribute_type": "creator", "attribute_value_mlt": [{"creatorNames": [{"creatorName": "平野, 陽一"}], "nameIdentifiers": [{"nameIdentifier": "409635", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "小野田, 淳次郎"}], "nameIdentifiers": [{"nameIdentifier": "409636", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "橋元, 保雄"}], "nameIdentifiers": [{"nameIdentifier": "409637", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "相原, 賢二"}], "nameIdentifiers": [{"nameIdentifier": "409638", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "HIRANO, Yoichi", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "409639", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "ONODA, Junjiro", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "409640", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "HASHIMOTO, Yasuo", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "409641", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "AIHARA, Kenji", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "409642", "nameIdentifierScheme": "WEKO"}]}]}, "item_files": {"attribute_name": "ファイル情報", "attribute_type": "file", "attribute_value_mlt": [{"accessrole": "open_date", "date": [{"dateType": "Available", "dateValue": "2020-01-24"}], "displaytype": "detail", "download_preview_message": "", "file_order": 0, "filename": "SA0125803.pdf", "filesize": [{"value": "1.2 MB"}], "format": "application/pdf", "future_date_message": "", "is_thumbnail": false, "licensetype": "license_free", "mimetype": "application/pdf", "size": 1200000.0, "url": {"label": "SA0125803.pdf", "url": "https://jaxa.repo.nii.ac.jp/record/32514/files/SA0125803.pdf"}, "version_id": "d80837cb-29eb-4790-bd43-b93c03262156"}]}, "item_language": {"attribute_name": "言語", "attribute_value_mlt": [{"subitem_language": "jpn"}]}, "item_resource_type": {"attribute_name": "資源タイプ", "attribute_value_mlt": [{"resourcetype": "departmental bulletin paper", "resourceuri": "http://purl.org/coar/resource_type/c_6501"}]}, "item_title": "\u003c論文\u003e曲げモーメントを受ける補強円筒殼の最小重量設計", "item_titles": {"attribute_name": "タイトル", "attribute_value_mlt": [{"subitem_title": "\u003c論文\u003e曲げモーメントを受ける補強円筒殼の最小重量設計"}]}, "item_type_id": "9", "owner": "1", "path": ["1890", "1910"], "permalink_uri": "https://jaxa.repo.nii.ac.jp/records/32514", "pubdate": {"attribute_name": "公開日", "attribute_value": "2015-03-26"}, "publish_date": "2015-03-26", "publish_status": "0", "recid": "32514", "relation": {}, "relation_version_is_last": true, "title": ["\u003c論文\u003e曲げモーメントを受ける補強円筒殼の最小重量設計"], "weko_shared_id": -1}
<論文>曲げモーメントを受ける補強円筒殼の最小重量設計
https://jaxa.repo.nii.ac.jp/records/32514
https://jaxa.repo.nii.ac.jp/records/32514931cf13e-59e6-4096-bef8-a91dda521599
名前 / ファイル | ライセンス | アクション |
---|---|---|
SA0125803.pdf (1.2 MB)
|
|
Item type | 紀要論文 / Departmental Bulletin Paper(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | <論文>曲げモーメントを受ける補強円筒殼の最小重量設計 | |||||
言語 | ||||||
言語 | jpn | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_6501 | |||||
資源タイプ | departmental bulletin paper | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Minimum Weight Design of Stiffened Cylindrical Shells under Pure Bending | |||||
著者 |
平野, 陽一
× 平野, 陽一× 小野田, 淳次郎× 橋元, 保雄× 相原, 賢二× HIRANO, Yoichi× ONODA, Junjiro× HASHIMOTO, Yasuo× AIHARA, Kenji |
|||||
著者所属 | ||||||
東京大学宇宙航空研究所 | ||||||
著者所属 | ||||||
東京大学宇宙航空研究所 | ||||||
著者所属 | ||||||
東京大学宇宙航空研究所 | ||||||
著者所属 | ||||||
東京大学宇宙航空研究所 | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Space and Aeronautical Science, University of Tokyo | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Space and Aeronautical Science, University of Tokyo | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Space and Aeronautical Science, University of Tokyo | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Space and Aeronautical Science, University of Tokyo | ||||||
出版者 | ||||||
出版者 | 東京大学宇宙航空研究所 | |||||
書誌情報 |
東京大学宇宙航空研究所報告 巻 15, 号 4, p. 865-878, 発行日 1979-11 |
|||||
抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | 曲げモーメント75 ton-mを受けるフレーム(円きょう)と縦通材で補強された直径2,440 mmの円筒殼の最小重量設計を行い,設計の妥当性を縮尺比1/3のモデルによる実験により確認した. | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | A method of structural optimization is applied in designing circular cylindrical shells under bending. The cylindrical shells are stiffened both longitudinally and circumferentially. A one-third scale model of the designed cylindrical shell has been made and tested to check the validity of the design. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0563-8100 | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AN00161914 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: SA0125803000 |