{"created":"2023-06-20T15:11:37.768879+00:00","id":41316,"links":{},"metadata":{"_buckets":{"deposit":"82abad4c-917f-4ef3-8f14-9f25de4560e8"},"_deposit":{"created_by":1,"id":"41316","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"41316"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00041316","sets":["1887:1893","1896:1898:1913:1915"]},"author_link":["489454","489451","489450","489452","489453","489455"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Multidisciplinary design optimization: Status and prospects in KHI"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2000-12","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"84","bibliographicPageStart":"79","bibliographicVolumeNumber":"46","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_3_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 7-9 Jun. 2000 東京 日本","subitem_description_type":"Other"}]},"item_3_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 7-9 Jun. 2000 Tokyo Japan","subitem_description_type":"Other"}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"多分野統合MDO(多分野総合最適化)技術の必要性は、コスト削減に対する要求および最近のコンピュータ技術の発展を背景に航空機製造分野で益々増大している。MDOは日本国内航空機メーカでは未だ未熟のように思われるが、主要な技術となりつつある。本稿では、MDOが適用できる航空機設計問題のいくつかの例について述べる。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The necessity of Multi-Disciplinary Optimization (MDO) technique has been increasing in the field of aircraft manufacturing against the background of the demand of reducing cost and the recent progress of computer technology. Though MDO seems still premature among aircraft manufacturers in Japan, it is becoming one of essential technologies. Some examples of aircraft design problems where MDO is applicable are shown here.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0028635015","subitem_description_type":"Other"}]},"item_3_description_33":{"attribute_name":"レポート番号","attribute_value_mlt":[{"subitem_description":"レポート番号: NAL SP-46","subitem_description_type":"Other"}]},"item_3_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"航空宇宙技術研究所"}]},"item_3_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"National Aerospace Laboratory (NAL)"}]},"item_3_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0289-260X","subitem_source_identifier_type":"ISSN"}]},"item_3_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_3_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"川崎重工業"},{"subitem_text_value":"川崎重工業"},{"subitem_text_value":"川崎重工業"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Kawasaki Heavy Industries Ltd"},{"subitem_text_language":"en","subitem_text_value":"Kawasaki Heavy Industries Ltd"},{"subitem_text_language":"en","subitem_text_value":"Kawasaki Heavy Industries Ltd"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"齋藤, 孝"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"嶋, 英志"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"生越, 博景"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Saito, Takashi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Shima, Eiji","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ogoshi, Hirokage","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":"nalsp0046015.pdf","filesize":[{"value":"1.2 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0046015.pdf","url":"https://jaxa.repo.nii.ac.jp/record/41316/files/nalsp0046015.pdf"},"version_id":"168634e9-0f08-4098-b176-cd3441a419ad"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"川崎重工業","subitem_subject_scheme":"Other"},{"subitem_subject":"多分野総合最適化","subitem_subject_scheme":"Other"},{"subitem_subject":"空力学","subitem_subject_scheme":"Other"},{"subitem_subject":"構造","subitem_subject_scheme":"Other"},{"subitem_subject":"装備","subitem_subject_scheme":"Other"},{"subitem_subject":"運用","subitem_subject_scheme":"Other"},{"subitem_subject":"統合設計","subitem_subject_scheme":"Other"},{"subitem_subject":"アンテナレドーム設計","subitem_subject_scheme":"Other"},{"subitem_subject":"ヘリコプタロータ","subitem_subject_scheme":"Other"},{"subitem_subject":"並列計算","subitem_subject_scheme":"Other"},{"subitem_subject":"最適空力設計","subitem_subject_scheme":"Other"},{"subitem_subject":"超音速輸送機","subitem_subject_scheme":"Other"},{"subitem_subject":"全機設計","subitem_subject_scheme":"Other"},{"subitem_subject":"MDO","subitem_subject_scheme":"Other"},{"subitem_subject":"Kawasaki Heavy Industries","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"multidisciplinary optimization","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamics","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"structure","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"equipment","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"operation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"integrated design","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"antenna radome design","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"helicopter rotor","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"parallel calculation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"optimal aerodynamic design","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"supersonic transport","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"total plane design","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"MDO","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":"technical report","resourceuri":"http://purl.org/coar/resource_type/c_18gh"}]},"item_title":"川崎重工業における統合シミュレーションの現状と今後の展望","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"川崎重工業における統合シミュレーションの現状と今後の展望"}]},"item_type_id":"3","owner":"1","path":["1893","1915"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"41316","relation_version_is_last":true,"title":["川崎重工業における統合シミュレーションの現状と今後の展望"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:03:22.549607+00:00"}