{"created":"2023-06-20T15:02:27.497467+00:00","id":31540,"links":{},"metadata":{"_buckets":{"deposit":"cca06750-1c71-46f0-8efe-e190248e7c89"},"_deposit":{"created_by":1,"id":"31540","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"31540"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00031540","sets":["1887:1890","1896:1898:1899:1910"]},"author_link":["404757","404755","404756","404754"],"item_9_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"On An Analysis of the Penetration of Rigid-Plastic Targets by Rigid Projectiles"}]},"item_9_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1974-12","bibliographicIssueDateType":"Issued"},"bibliographicIssueNumber":"4_B","bibliographicPageEnd":"834","bibliographicPageStart":"829","bibliographicVolumeNumber":"10","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":"飛行体が固体に貫入する問題を剛塑性体近似に基づく上界定理を用いて解析した。飛行体が平板に貫入し,突き抜けに到る過程を3つの段階に分けて考え,それぞれについて適当な可容速度場を求めた。この手法により,飛行体の貫入抵抗,突き抜けに要するエネルギ等について簡単に扱える解析的公式を導出した。","subitem_description_type":"Abstract"}]},"item_9_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The problem on the penetration of rigid-plastic targets by rigid projectiles is theoretically studied. Slip line theory is used and the analysis is based on the upper bound theorem. The process of the penetration of plate targets is classified into three stages by the depth of penetration. By the use of the proper kinematically admissible field in each stage, simple analytical formulae for the calculation of the resistance and the energy required for the penetration are obtained.","subitem_description_type":"Other"}]},"item_9_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: SA0124458000","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 Aeroautical Science University of Tokyo"},{"subitem_text_language":"en","subitem_text_value":"Institute of Space and Aeroautical Science University of Tokyo"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"河田, 幸三"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"塩谷, 義"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"KAWATA, Kozo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"SHIOYA, Tadashi","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":"2020-01-23"}],"displaytype":"detail","filename":"SA0124458.pdf","filesize":[{"value":"275.8 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"SA0124458.pdf","url":"https://jaxa.repo.nii.ac.jp/record/31540/files/SA0124458.pdf"},"version_id":"a942c182-2459-455c-8ca2-695214f6ab25"}]},"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":"高速飛行体の固体への衝撃貫入の解析について","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"高速飛行体の固体への衝撃貫入の解析について"}]},"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":"31540","relation_version_is_last":true,"title":["高速飛行体の固体への衝撃貫入の解析について"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T00:57:11.561230+00:00"}