{"created":"2023-06-20T15:03:25.496811+00:00","id":32632,"links":{},"metadata":{"_buckets":{"deposit":"64cae243-d49a-419e-9656-dafd551c12c3"},"_deposit":{"created_by":1,"id":"32632","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"32632"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00032632","sets":["1887:1890","1896:1898:1899:1910"]},"author_link":["410458","410460","410459","410457"],"item_9_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Dynamic Buckling of Cylindrical Shells : Energy Approach and Simplified Models"}]},"item_9_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1981-03","bibliographicIssueDateType":"Issued"},"bibliographicIssueNumber":"1_B","bibliographicPageEnd":"402","bibliographicPageStart":"357","bibliographicVolumeNumber":"17","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":"本研究は,衝撃軸圧縮荷重を受ける円筒殼を例題として,動的挫屈現象の機構を解明しようとするものである.エネルギー的考察により,「動的挫屈荷重のエネルギー的限界値」の概念を導入し,それと運動方程式の数値積分により得られる動的挫屈荷重とを比較検討する事により,エネルギー的限界値の持つ意味を明確にする.更に上述の解析結果を基礎として,質量-ばね-リンクからなる二種類の単純化モデルを考案し,その挙動を解析する.特に線形ばねのみを用いた単純化モデルに於ては,モデル構成要素の持つ物理的意味が従来のモデルに比して極めて明確となる事を示す.","subitem_description_type":"Abstract"}]},"item_9_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The aim of the present paper is to clarify the mechanism of dynamic buckling through analysing the behavior of cylindrical shells under axial impulsive loading. An energy approach is used to derive the critical value of the dynamic buckling load. The physical meaning of this bound is clarified and illustrated through numerical integration of the equations of motion and comparison of the results. On the basis of this analysis, the authors construct two simplified models and analyse their behavior. One of these models uses only linear springs, each of which provides for one corresponding mechanical property a simple and clear representation which is not available from the custamary nonlinear-spring models.","subitem_description_type":"Other"}]},"item_9_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: SA0125973000","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_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"}]},"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"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"木部, 勢至朗"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"砂川, 恵"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"KIBE, Seishiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"SUNAKAWA, Megumi","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":"2020-01-24"}],"displaytype":"detail","filename":"SA0125973.pdf","filesize":[{"value":"1.5 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"SA0125973.pdf","url":"https://jaxa.repo.nii.ac.jp/record/32632/files/SA0125973.pdf"},"version_id":"14672f1b-8578-4133-bbd2-23f730f3a7d9"}]},"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":"<論文>円筒殼の動的挫屈に於るエネルギー的考察と単純化モデル","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"<論文>円筒殼の動的挫屈に於るエネルギー的考察と単純化モデル"}]},"item_type_id":"9","owner":"1","path":["1890","1910"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"32632","relation_version_is_last":true,"title":["<論文>円筒殼の動的挫屈に於るエネルギー的考察と単純化モデル"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T00:27:30.752558+00:00"}