{"created":"2023-06-19T12:44:31.025121+00:00","id":3992,"links":{},"metadata":{"_buckets":{"deposit":"934e9389-4590-4c88-b565-9a50420d202f"},"_deposit":{"created_by":3,"id":"3992","owners":[3],"pid":{"revision_id":0,"type":"depid","value":"3992"},"status":"published"},"_oai":{"id":"oai:tokyo-metro-u.repo.nii.ac.jp:00003992","sets":["1647:634:647"]},"author_link":["12247","12248","12249","12250","12251","12252"],"control_number":"3992","item_9_alternative_title_21":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"Efficient Geometry Representation of Airframe Based on simulation"}]},"item_9_biblio_info_9":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2010-11","bibliographicIssueDateType":"Issued"}}]},"item_9_creator_2":{"attribute_name":"著者(ヨミ)","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"キヤムラ, ユタカ"}],"nameIdentifiers":[{"nameIdentifier":"12249","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"カナザキ, マサヒロ"}],"nameIdentifiers":[{"nameIdentifier":"12250","nameIdentifierScheme":"WEKO"}]}]},"item_9_creator_3":{"attribute_name":"著者別名","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"Kiyamura, Yutaka"}],"nameIdentifiers":[{"nameIdentifier":"12251","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Kanazaki, Masahiro"}],"nameIdentifiers":[{"nameIdentifier":"12252","nameIdentifierScheme":"WEKO"}]}]},"item_9_description_4":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"In this presentation, a geometry representation method for a wing/fuselage configuration is discussed for arbitrary civil aircrafts. For a wing design, five airfoil geometries are defined using modified PASEC airfoil representation for the taper wing which has a kink. In addition, the positions and the sizes of each airfoil, aspect ratio, dihedral angle and wash-out can be changed. Fuselage geometry is basically defined as a tube. To achieve more realistic design, polynomial functions are used to represent the geometry of fuselage around the wing root, the fuselage nose and the tail. After the solid model of the wing/fuselage, the unstructured mesh is generated for flow simulation. To investigate proposed methods, parameter identification with existing transonic aircrafts' model is carried out. Their geometries and flow fields are investigated. This result suggests that the proposed methods can represent various geometries well and the fuselage geometry around the wing root is effective to the aerodynamic performance. Thus, the design representation proposed here has possibility to be useful for the aircraft design using data mining.","subitem_description_type":"Abstract"}]},"item_9_description_42":{"attribute_name":"資源タイプ","attribute_value_mlt":[{"subitem_description":"postprint","subitem_description_type":"Other"}]},"item_9_description_5":{"attribute_name":"内容記述","attribute_value_mlt":[{"subitem_description":"精密工学会 Design Symposium (発表No: dss10-0057)","subitem_description_type":"Other"}]},"item_9_publisher_35":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"精密工学会"}]},"item_9_rights_15":{"attribute_name":"権利","attribute_value_mlt":[{"subitem_rights":"精密工学会"}]},"item_9_version_type_18":{"attribute_name":"著者版フラグ","attribute_value_mlt":[{"subitem_version_resource":"http://purl.org/coar/version/c_ab4af688f83e57aa","subitem_version_type":"AM"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"木矢村, 豊"}],"nameIdentifiers":[{"nameIdentifier":"12247","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"金崎, 雅博"}],"nameIdentifiers":[{"nameIdentifier":"12248","nameIdentifierScheme":"WEKO"}]}]},"item_files":{"attribute_name":"ファイル情報","attribute_type":"file","attribute_value_mlt":[{"accessrole":"open_date","date":[{"dateType":"Available","dateValue":"2016-08-04"}],"displaytype":"detail","filename":"10165-001.pdf","filesize":[{"value":"1.0 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"10165-001.pdf","url":"https://tokyo-metro-u.repo.nii.ac.jp/record/3992/files/10165-001.pdf"},"version_id":"b0828981-8011-42cf-87a3-3e4a53adcd8e"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"CFD","subitem_subject_scheme":"Other"},{"subitem_subject":"Transonic wing","subitem_subject_scheme":"Other"},{"subitem_subject":"Multi-disciplinary design","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":"シミュレーションによる高効率航空機形状設計法","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"シミュレーションによる高効率航空機形状設計法","subitem_title_language":"ja"}]},"item_type_id":"9","owner":"3","path":["647"],"pubdate":{"attribute_name":"PubDate","attribute_value":"2011-09-28"},"publish_date":"2011-09-28","publish_status":"0","recid":"3992","relation_version_is_last":true,"title":["シミュレーションによる高効率航空機形状設計法"],"weko_creator_id":"3","weko_shared_id":-1},"updated":"2023-07-25T04:42:21.631361+00:00"}