{"created":"2023-06-20T15:08:04.431679+00:00","id":37462,"links":{},"metadata":{"_buckets":{"deposit":"ba6d9200-864e-4bd5-882e-ffebd7ff9be7"},"_deposit":{"created_by":1,"id":"37462","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"37462"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00037462","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["480901","480904","480906","480907","480908","480903","480902","480905"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Drop test simulation of simplified structural models of aircraft fuselage"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1999-12","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"196","bibliographicPageStart":"191","bibliographicVolumeNumber":"44","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所特別資料"},{"bibliographic_title":"Special Publication of National Aerospace Laboratory","bibliographic_titleLang":"en"}]}]},"item_5_description_14":{"attribute_name":"会議概要（会議名, 開催地, 会期, 主催者等）","attribute_value_mlt":[{"subitem_description":"航空宇宙技術研究所 16-18 Jun. 1999 東京 日本","subitem_description_type":"Other"}]},"item_5_description_15":{"attribute_name":"会議概要（会議名, 開催地, 会期, 主催者等）（英）","attribute_value_mlt":[{"subitem_description":"National Aerospace Laboratory 16-18 Jun. 1999 Tokyo Japan","subitem_description_type":"Other"}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"航空機の墜落事故に際し搭乗者の生存率を向上させるためには、搭乗者の周りの衝撃環境を人体が耐えることの出来る許容レベル以下に抑えなければならない。本研究の目的は、衝撃エネルギーの吸収による搭乗者の生存率向上の観点から、胴体構造の衝撃挙動を実験と数値計算により検討することである。本論文ではその予備段階として簡単化した胴体下部構造に関して落下衝撃実験を行ったので、その結果を報告した。また構造モデルに対応した数値解析モデルを開発し、有限要素解析コードLS-DYNA3Dを使って解析した。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"For ensuring occupant's survivability in case of crash accident of aircraft, the impact environment around the occupants must be less severe than an allowable level below which the human body can endure. This research aims to examine the crash behavior of fuselage structure both by tests and numerical analysis in view of the impact energy absorption and occupant's survivability. In this paper, some results on simplified structural models of the sub-floor fuselage structure, which were subjected to vertical drop test as the preliminary stage of examination, are presented. A numerical model corresponding to the structural model was developed and analyzed using a finite element analysis code, LS-DYNA3D.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0001961029","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: NAL SP-44","subitem_description_type":"Other"}]},"item_5_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"航空宇宙技術研究所"}]},"item_5_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"National Aerospace Laboratory (NAL)"}]},"item_5_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0289-260X","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":"AN10097345","subitem_source_identifier_type":"NCID"}]},"item_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"法政大学 工学部　システム制御工学科"},{"subitem_text_value":"航空宇宙技術研究所 構造材料総合研究グループ"},{"subitem_text_value":"航空宇宙技術研究所 構造材料総合研究グループ"},{"subitem_text_value":"航空宇宙技術研究所 構造材料総合研究グループ"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Hosei University Department of Systems Control Engineering, College of Engineering"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Structures and Materials Research Center"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Structures and Materials Research Center"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Structures and Materials Research Center"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"細川, 剛史"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"熊倉, 郁夫"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"峯岸, 正勝"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"岩崎, 和夫"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hosokawa, Takefumi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kumakura, Ikuo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Minegishi, Masakatsu","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Iwasaki, Kazuo","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":"2020-02-10"}],"displaytype":"detail","filename":"nalsp0044029.pdf","filesize":[{"value":"1.3 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0044029.pdf","url":"https://jaxa.repo.nii.ac.jp/record/37462/files/nalsp0044029.pdf"},"version_id":"da2fb136-9798-4dc7-867d-f64ac31603f4"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"落下衝撃","subitem_subject_scheme":"Other"},{"subitem_subject":"垂直落下実験","subitem_subject_scheme":"Other"},{"subitem_subject":"衝撃エネルギー吸収","subitem_subject_scheme":"Other"},{"subitem_subject":"搭乗者生存率","subitem_subject_scheme":"Other"},{"subitem_subject":"応力分布","subitem_subject_scheme":"Other"},{"subitem_subject":"構造変形","subitem_subject_scheme":"Other"},{"subitem_subject":"航空機胴体構造","subitem_subject_scheme":"Other"},{"subitem_subject":"胴体下部構造","subitem_subject_scheme":"Other"},{"subitem_subject":"簡単化構造模型","subitem_subject_scheme":"Other"},{"subitem_subject":"有限要素解析","subitem_subject_scheme":"Other"},{"subitem_subject":"drop impact","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"vertical drop impact test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"impact energy absorption","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"occupant's survivability","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"stress distribution","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"structure deformation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aircraft fuselage structure","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"sub floor fuselage structure","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"simplified suructural model","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"finite element analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"}]},"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":"conference paper","resourceuri":"http://purl.org/coar/resource_type/c_5794"}]},"item_title":"航空機胴体下部構造モデルの衝撃数値シミュレーション","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"航空機胴体下部構造モデルの衝撃数値シミュレーション"}]},"item_type_id":"5","owner":"1","path":["1891","1915"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"37462","relation_version_is_last":true,"title":["航空機胴体下部構造モデルの衝撃数値シミュレーション"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:18:21.939485+00:00"}