{"created":"2023-07-25T09:16:18.414719+00:00","id":16442,"links":{},"metadata":{"_buckets":{"deposit":"142ca923-de4e-4d67-a9e2-3f0912fe7762"},"_deposit":{"created_by":19,"id":"16442","owners":[19],"pid":{"revision_id":0,"type":"depid","value":"16442"},"status":"published"},"_oai":{"id":"oai:toyama.repo.nii.ac.jp:00016442","sets":["496:556:557:558"]},"author_link":["23957","169589","169591","169590"],"item_2_alternative_title_19":{"attribute_name":"その他（別言語等）のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"Modification of PARSEC Airfoil Representation and Investigation of Design Performance"}]},"item_2_biblio_info_7":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2011-01-05","bibliographicIssueDateType":"Issued"},"bibliographicIssueNumber":"684","bibliographicPageEnd":"26","bibliographicPageStart":"24","bibliographicVolumeNumber":"59","bibliographic_titles":[{"bibliographic_title":"日本航空宇宙学会論文集 = Journal of the Japan Society for Aeronautical and Space Sciences"},{"bibliographic_title":"JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES"}]}]},"item_2_description_15":{"attribute_name":"フォーマット","attribute_value_mlt":[{"subitem_description":"application/pdf","subitem_description_type":"Other"}]},"item_2_description_4":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"The original PARSEC (PARametric SECtion) method can satisfactorily solve the optimization problems involving transonic airfoils by using a few design variables. However, it is difficult to apply this method to the design of airfoils under other conditions such as supersonic flow and low Reynolds number flow. To solve various airfoil design problems by using a few design variables and the PARSEC representation, a modified PARSEC representation is proposed. The capability of the proposed modified representation to solve unknown real-world design problems is investigated; the proposed representation is used along with multi-objective genetic algorithms to solve two types of problems. One is the design of a conventional transonic airfoil that is to be used in the Earth's atmosphere; the other is the design of an airfoil that is to be used in the Martian atmosphere. To evaluate the aerodynamic performance of the airfoils, the structured Navier-Stokes solver is used. The results indicate that better solutions can be obtained by using the proposed PARSEC modification than by using the original PARSEC representation, especially in the Martian atmosphere.","subitem_description_type":"Abstract"}]},"item_2_description_40":{"attribute_name":"資源タイプ(DSpace)","attribute_value_mlt":[{"subitem_description":"Article","subitem_description_type":"Other"}]},"item_2_description_6":{"attribute_name":"引用","attribute_value_mlt":[{"subitem_description":"日本航空宇宙学会論文集 = Journal of the Japan Society for Aeronautical and Space Sciences 59(684), 24-26.(2011)","subitem_description_type":"Other"}]},"item_2_full_name_3":{"attribute_name":"著者別名","attribute_value_mlt":[{"nameIdentifiers":[{"nameIdentifier":"169589","nameIdentifierScheme":"WEKO"},{"nameIdentifier":"9000003743163","nameIdentifierScheme":"CiNii ID","nameIdentifierURI":"http://ci.nii.ac.jp/nrid/9000003743163"},{"nameIdentifier":"10392838","nameIdentifierScheme":"e-Rad","nameIdentifierURI":"https://nrid.nii.ac.jp/nrid/1000010392838"}],"names":[{"name":"Kanazaki, Masahiro"}]},{"nameIdentifiers":[{"nameIdentifier":"169590","nameIdentifierScheme":"WEKO"},{"nameIdentifier":"9000018746870","nameIdentifierScheme":"CiNii ID","nameIdentifierURI":"http://ci.nii.ac.jp/nrid/9000018746870"}],"names":[{"name":"Yotsuya, Tomonori"}]},{"nameIdentifiers":[{"nameIdentifier":"169591","nameIdentifierScheme":"WEKO"},{"nameIdentifier":"9000018600355","nameIdentifierScheme":"CiNii ID","nameIdentifierURI":"http://ci.nii.ac.jp/nrid/9000018600355"}],"names":[{"name":"Nara, Takuya"}]},{"nameIdentifiers":[{"nameIdentifier":"23957","nameIdentifierScheme":"WEKO"},{"nameIdentifier":"1000040332514","nameIdentifierScheme":"CiNii ID","nameIdentifierURI":"http://ci.nii.ac.jp/nrid/1000040332514"},{"nameIdentifier":"40332514","nameIdentifierScheme":"e-Rad","nameIdentifierURI":"https://nrid.nii.ac.jp/nrid/1000040332514"}],"names":[{"name":"Matsushima, Kisa"}]}]},"item_2_publisher_33":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"一般社団法人 日本航空宇宙学会"},{"subitem_publisher":"THE JAPAN SOCIETY AERONAUTICAL AND SPACE SCIENCES"}]},"item_2_relation_12":{"attribute_name":"DOI","attribute_value_mlt":[{"subitem_relation_type":"isIdenticalTo","subitem_relation_type_id":{"subitem_relation_type_id_text":"10.2322/jjsass.59.24","subitem_relation_type_select":"DOI"}}]},"item_2_relation_29":{"attribute_name":"論文ID（NAID）","attribute_value_mlt":[{"subitem_relation_type":"isIdenticalTo","subitem_relation_type_id":{"subitem_relation_type_id_text":"10028049062","subitem_relation_type_select":"NAID"}}]},"item_2_rights_13":{"attribute_name":"権利","attribute_value_mlt":[{"subitem_rights":"Copyright 2011 The Japan Society for Aeronautical and Space Sciences."}]},"item_2_source_id_10":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AA11307372","subitem_source_identifier_type":"NCID"}]},"item_2_source_id_8":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"13446460","subitem_source_identifier_type":"ISSN"}]},"item_2_version_type_16":{"attribute_name":"著者版フラグ","attribute_value_mlt":[{"subitem_version_resource":"http://purl.org/coar/version/c_970fb48d4fbd8a85","subitem_version_type":"VoR"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"金崎, 雅博"}],"nameIdentifiers":[{},{},{}]},{"creatorNames":[{"creatorName":"四谷, 智義"}],"nameIdentifiers":[{},{}]},{"creatorNames":[{"creatorName":"奈良, 拓矢"}],"nameIdentifiers":[{},{}]},{"creatorNames":[{"creatorName":"松島, 紀佐"}],"nameIdentifiers":[{},{},{}]}]},"item_files":{"attribute_name":"ファイル情報","attribute_type":"file","attribute_value_mlt":[{"accessrole":"open_date","date":[{"dateType":"Available","dateValue":"2018-08-21"}],"displaytype":"detail","filename":"NihonKokuUchuGakkai_59_684_024to026_Matsushima.pdf","filesize":[{"value":"532.9 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"NihonKokuUchuGakkai_59_684_024to026_Matsushima","url":"https://toyama.repo.nii.ac.jp/record/16442/files/NihonKokuUchuGakkai_59_684_024to026_Matsushima.pdf"},"version_id":"e47b61ca-64a2-4746-9f5e-a904cbdc70f2"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"Airfoil Representation","subitem_subject_scheme":"Other"},{"subitem_subject":"Genetic Algorithms","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD","subitem_subject_scheme":"Other"},{"subitem_subject":"Airfoil Representation","subitem_subject_scheme":"Other"},{"subitem_subject":"Genetic Algorithms","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD","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":"journal article","resourceuri":"http://purl.org/coar/resource_type/c_6501"}]},"item_title":"PARSEC翼型表現法の修正手法と表現性能検証","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"PARSEC翼型表現法の修正手法と表現性能検証"},{"subitem_title":"Modification of PARSEC Airfoil Representation and Investigation of Design Performance","subitem_title_language":"en"}]},"item_type_id":"2","owner":"19","path":["558"],"pubdate":{"attribute_name":"公開日","attribute_value":"2018-08-21"},"publish_date":"2018-08-21","publish_status":"0","recid":"16442","relation_version_is_last":true,"title":["PARSEC翼型表現法の修正手法と表現性能検証"],"weko_creator_id":"19","weko_shared_id":-1},"updated":"2023-07-25T12:46:20.725184+00:00"}