{"created":"2023-06-20T15:11:37.717895+00:00","id":41315,"links":{},"metadata":{"_buckets":{"deposit":"ad661838-8374-4fcb-9725-6774705920aa"},"_deposit":{"created_by":1,"id":"41315","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"41315"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00041315","sets":["1887:1893","1896:1898:1913:1915"]},"author_link":["489448","489449","489446","489447"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"The present state and future views of multi-integrated CFD simulation on MHI Nagoya Aerospace Works"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2000-12","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"78","bibliographicPageStart":"73","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":"他の解析と連合したCFD(計算流体力学)シミュレーションは飛行の安全および実験の安全確保のためにメーカにとって必要である。本稿では、当社でこれまでに行ったアプリケーションの計算例を示す。最初のアプリケーションは、他体からの分離およびヘリコプタブレードの回転をシミュレートする運動力学と連成していた。次のアプリケーションは、HSI(高速衝撃)雑音強度を得るための音響解析を行った。最後に、宇宙船の変形を把握するため構造解析を行った。力学的構造問題を伴うCFD解析は、産官学の共同研究として強化されることを期待している。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"CFD (Computational Fluid Dynamics) simulation associated with other analysis is necessary for the makers in order to keep flight and experiment safety. This paper shows several applications that were calculated so far in the company. First application is coupled with motion dynamics to simulate the separation from another body and the rotation of helicopter blades. Next one is done with the acoustics analysis to obtain the HSI (High Speed Impulsive) noise intensity. Last one is done with the structure analysis to capture the transformation of the space plane. CFD analysis associated with dynamic structure problems will be anticipated to be intensified as the collaborative work of the industries, government and universities.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0028635014","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":"三菱重工業"},{"subitem_text_value":"菱友計算"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Mitsubishi Heavy Industries Ltd"},{"subitem_text_language":"en","subitem_text_value":"Ryoyu Keisan Co Ltd"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"海田, 武司"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"渡邉, 直樹"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kaiden, Takeshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Watanabe, Naoki","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":"nalsp0046014.pdf","filesize":[{"value":"2.2 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0046014.pdf","url":"https://jaxa.repo.nii.ac.jp/record/41315/files/nalsp0046014.pdf"},"version_id":"31c821c6-8263-40ae-869b-3e45fd5455e0"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"三菱名航","subitem_subject_scheme":"Other"},{"subitem_subject":"計算流体力学","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD","subitem_subject_scheme":"Other"},{"subitem_subject":"空力設計","subitem_subject_scheme":"Other"},{"subitem_subject":"渦度等値面","subitem_subject_scheme":"Other"},{"subitem_subject":"多分野総合シミュレーション","subitem_subject_scheme":"Other"},{"subitem_subject":"超音速実験機","subitem_subject_scheme":"Other"},{"subitem_subject":"ヘリコプタブレード運動","subitem_subject_scheme":"Other"},{"subitem_subject":"衝撃音解析","subitem_subject_scheme":"Other"},{"subitem_subject":"ブレードCFD解析","subitem_subject_scheme":"Other"},{"subitem_subject":"静的空力弾性解析","subitem_subject_scheme":"Other"},{"subitem_subject":"表面圧力分布","subitem_subject_scheme":"Other"},{"subitem_subject":"構造変形解析","subitem_subject_scheme":"Other"},{"subitem_subject":"HSI","subitem_subject_scheme":"Other"},{"subitem_subject":"高速衝突","subitem_subject_scheme":"Other"},{"subitem_subject":"MHI Nagoya Aerospace Works","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"computational fluid dynamics","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic design","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"vorticity isosurface","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"multidisciplinary simulation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"supersonic experimental plane","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"helicopter blade motion","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"sonic boom analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"blade CFD analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"static aeroelasticity analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"surface pressure distribution","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"structural deformation analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"HSI","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"high speed impact","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":"三菱名航におけるCFD統合シミュレーションの現状と展望","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"三菱名航におけるCFD統合シミュレーションの現状と展望"}]},"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":"41315","relation_version_is_last":true,"title":["三菱名航におけるCFD統合シミュレーションの現状と展望"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:03:23.546543+00:00"}