{"created":"2023-06-20T14:36:14.075877+00:00","id":2546,"links":{},"metadata":{"_buckets":{"deposit":"77974f00-ae5e-4d81-b1e5-bc5936161c63"},"_deposit":{"created_by":1,"id":"2546","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"2546"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00002546","sets":["1887:1893","9:1090:1186:1201"]},"author_link":["7150","7156","7152","7148","7151","7153","7149","7155","7158","7160","7159","7157","7161","7147","7154","7162"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Database for Aerodynamic Design of Supersonic Transport (NEXST-DB)"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2012-01-31","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"30","bibliographicPageStart":"1","bibliographicVolumeNumber":"JAXA-RM-11-009","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構研究開発資料"},{"bibliographic_title":"JAXA Research and Development Memorandum","bibliographic_titleLang":"en"}]}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"次世代超音速旅客機の研究開発として進められた小型超音速実験機(NEXST)プログラムにおいて蓄積された空力データを収録した超音速機空力設計データベース(NEXST-DB)を構築した．インターネット公開型のデータベースであり，Web上で図示機能やテキストデータのダウンロード機能を充実させ，正確なデータが迅速に利用できるようにした．本NEXST-DBには空力データ，機体形状データ，空力設計ツール，そして対外発表資料を掲載・公開している．空力データには，NEXST-1の飛行実験や，CFD解析，風洞試験，境界層遷移解析結果を掲載し，機体形状データはCAD形式の形状ファイルが利用できるようにした．空力設計ツールは，NEXST-1の空力設計に用いた抵抗低減設計ツールやCFD逆問題設計ツールを掲載し，利用の多様化を図った．掲載内容や機能，利用方法の詳細についてまとめた．","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"A database for aerodynamic design of the supersonic transport (NEXST-DB) was constructed by JAXA. Many kind of aerodynamic data uploaded on the NEXST-DB were accumulated from the NEXST program. The uploaded data on the NEXST-DB consisted by aerodynamic results, airplane geometries, aerodynamic design tools and publications. A fl ight test, CFD analysis, wind tunnel test and the boundary layer transition analysis results obtained from the NEXST-1 project were mainly uploaded as the aerodynamic results. The aerodynamic design tools were developed on the project and used for designing of the NEXST-1 airplane. All of the aerodynamic data and tools uploaded on the NEXST-DB can freely be downloaded from the website. The detail information of the publications related to the NEXST program was also introduced.","subitem_description_type":"Other"}]},"item_3_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_3_description_19":{"attribute_name":"内容記述（英）","attribute_value_mlt":[{"subitem_description":"Physical characteristics: Original contains color illustrations","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0065139000","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: JAXA-RM-11-009","subitem_description_type":"Other"}]},"item_3_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙航空研究開発機構(JAXA)"}]},"item_3_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Japan Aerospace Exploration Agency (JAXA)"}]},"item_3_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"1349-1121","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":"AA11983593","subitem_source_identifier_type":"NCID"}]},"item_3_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 (JAXA)"},{"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 (JAXA)"},{"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 (JAXA)"},{"subitem_text_value":"三向ソフトウェア開発"},{"subitem_text_value":"東京ビジネスサービス"},{"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 (JAXA)"},{"subitem_text_value":"菱友システムズ"},{"subitem_text_value":"菱友システムズ"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Supersonic Transport Team, Aviation Program Group, Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Supersonic Transport Team, Aviation Program Group, Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Supersonic Transport Team, Aviation Program Group, Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Sanko Soft"},{"subitem_text_language":"en","subitem_text_value":"Tokyo Business Service"},{"subitem_text_language":"en","subitem_text_value":"Supersonic Transport Team, Aviation Program Group, Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Ryoyu Systems"},{"subitem_text_language":"en","subitem_text_value":"Ryoyu Systems"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"郭, 東潤"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"徳川, 直子"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"吉田, 憲司"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"石川, 敬掲"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"上田, 良稲"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"伊藤, 健"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"黒田, 文武"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"大平, 啓介"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kwak, Dong-Youn","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Tokugawa, Naoko","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yoshida, Kenji","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ishikawa, Hiroaki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ueda, Yoshine","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ito, Takeshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kuroda, Fumitake","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ohira, Keisuke","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":"2020-01-15"}],"displaytype":"detail","filename":"65139000.pdf","filesize":[{"value":"4.8 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"65139000.pdf","url":"https://jaxa.repo.nii.ac.jp/record/2546/files/65139000.pdf"},"version_id":"75ce57d6-a3b6-405c-aa98-31c517daa90d"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"Database","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Supersonic Transport","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Aerodynamics","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":"超音速機空力設計データベース(NEXST-DB)の構築","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"超音速機空力設計データベース(NEXST-DB)の構築"}]},"item_type_id":"3","owner":"1","path":["1201","1893"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"2546","relation_version_is_last":true,"title":["超音速機空力設計データベース(NEXST-DB)の構築"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T09:20:22.955826+00:00"}