{"created":"2023-06-20T14:38:49.926870+00:00","id":5449,"links":{},"metadata":{"_buckets":{"deposit":"1406b3a5-e918-4738-8516-25e0f1a9f7d5"},"_deposit":{"created_by":1,"id":"5449","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"5449"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00005449","sets":["1887:1891","9:789:956:965"]},"author_link":["26450","26451"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Introduction of aerodynamic design of a silent supersonic technology demonstrator"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2009-02-27","bibliographicIssueDateType":"Issued"},"bibliographicVolumeNumber":"JAXA-SP-08-008","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構特別資料: 小型超音速実験機（ロケット実験機）飛行実験データ解析完了報告"},{"bibliographic_title":"JAXA Special Publication","bibliographic_titleLang":"en"}]}]},"item_5_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":"小型超音速実験機（ロケット実験機）飛行実験データ解析完了報告会(平成20年7月10日. 東京大学山上会館)","subitem_description_type":"Other"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"JAXA's planned scaled low-boom demonstrator project and its aerodynamic design in conceptual design phase are introduced. For the demonstration of low sonic-boom design concepts and design technology, this demonstrator named Silent SuperSonic Technology Demonstrator (S3TD) is designed using JAXA's computer-based aerodynamic design tools for low-drag and low-boom configuration. A multidisciplinary design exploration, in which the aerodynamic performance estimated by an unstructured Euler CFD code, sonic-boom intensity, and structural constraints are taken into account, is applied to the design of the demonstrator as well as an aerodynamic conceptual design tool based on a low-fidelity panel method. Several design cycles are conducted through the validation process for mission requirement with many CFD analyses and wind-tunnel tests.","subitem_description_type":"Other"}]},"item_5_description_18":{"attribute_name":"内容記述","attribute_value_mlt":[{"subitem_description":"形態: カラー図版あり","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0064239013","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-08-008","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":"宇宙航空研究開発機構航空プログラムグループ超音速機チーム"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Aviation Program Group, Japan Aerospace Exploration Agency (JAXA)"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"牧野, 好和"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Makino, Yoshikazu","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":"64239013.pdf","filesize":[{"value":"6.9 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"64239013.pdf","url":"https://jaxa.repo.nii.ac.jp/record/5449/files/64239013.pdf"},"version_id":"4c816ca3-abcf-4958-954f-7f2de110dcdc"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"Aerodynamic Design, Optimization, Supersonic Transport, Sonic-Boom","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":"静粛超音速研究機の空力設計の概要","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"静粛超音速研究機の空力設計の概要"}]},"item_type_id":"5","owner":"1","path":["965","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"5449","relation_version_is_last":true,"title":["静粛超音速研究機の空力設計の概要"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T08:14:50.480305+00:00"}