{"created":"2023-06-20T14:39:48.710690+00:00","id":6615,"links":{},"metadata":{"_buckets":{"deposit":"5c8f7e25-cd2e-4468-ba74-41208cbd0061"},"_deposit":{"created_by":1,"id":"6615","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"6615"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00006615","sets":["1887:1891","9:789:1085:1366"]},"author_link":["33871","33868","33869","33870"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"MHI activities on aeroelastic analysis"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2004-03-25","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"80","bibliographicPageStart":"75","bibliographicVolumeNumber":"JAXA-SP-03-002","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構特別資料: 航空宇宙数値シミュレーション技術シンポジウム2003論文集"},{"bibliographic_title":"JAXA Special Publication: Proceedings of Aerospace Numerical Simulation Symposium 2003","bibliographic_titleLang":"en"}]}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"MHI activities on aeroelasticity and the associated fields are presented. MHI has conducted many types of aeroelastic analysis throughout the development of aircraft in the past decades. The transonic dip phenomenon is one of the most important items in the aeroelasticity field and cannot be analyzed by the linear aerodynamics tools commonly used in the aircraft design. The recent progress in the time-marching method that calculates the flow field around the airfoil in the time domain enables solving the transonic dip by the analysis. In this paper, two analysis examples using USTF3 developed at NAL are presented that studied the transonic flutter properties of the high-aspect-ratio transport wing and SST wing, both of which were done in the design phase at MHI.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0047427014","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: JAXA-SP-03-002","subitem_description_type":"Other"}]},"item_5_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙航空研究開発機構"}]},"item_5_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Japan Aerospace Exploration Agency (JAXA)"}]},"item_5_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"1349-113X","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":"AA11984031","subitem_source_identifier_type":"NCID"}]},"item_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"三菱重工業"},{"subitem_text_value":"日本航空機開発協会"}]},"item_5_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":"Japan Aircraft Development Corporation"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"野村, 隆之"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"柳川, 祐輝"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nomura, Takayuki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yanagawa, Hiroki","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":"2020-01-16"}],"displaytype":"detail","filename":"47427014.pdf","filesize":[{"value":"588.8 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"47427014.pdf","url":"https://jaxa.repo.nii.ac.jp/record/6615/files/47427014.pdf"},"version_id":"17fbad16-9ca6-4ba1-b240-7a33215a342a"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"空力弾性","subitem_subject_scheme":"Other"},{"subitem_subject":"航空機設計","subitem_subject_scheme":"Other"},{"subitem_subject":"遷音速飛行","subitem_subject_scheme":"Other"},{"subitem_subject":"遷音速フラッタ","subitem_subject_scheme":"Other"},{"subitem_subject":"SST","subitem_subject_scheme":"Other"},{"subitem_subject":"境界層剥離","subitem_subject_scheme":"Other"},{"subitem_subject":"高アスペクト比翼","subitem_subject_scheme":"Other"},{"subitem_subject":"超音速飛行","subitem_subject_scheme":"Other"},{"subitem_subject":"aeroelasticity","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aircraft design","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"transonic flight","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"transonic flutter","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"SST","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"boundary layer separation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"high aspect ratio wing","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"supersonic flight","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":"MHIにおける空力弾性応答解析について","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"MHIにおける空力弾性応答解析について"}]},"item_type_id":"5","owner":"1","path":["1366","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"6615","relation_version_is_last":true,"title":["MHIにおける空力弾性応答解析について"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T07:52:23.019049+00:00"}