{"created":"2023-06-20T15:08:00.080396+00:00","id":37386,"links":{},"metadata":{"_buckets":{"deposit":"287cbb2c-1a6a-4549-ade6-3d19084eefec"},"_deposit":{"created_by":1,"id":"37386","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"37386"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00037386","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["480488","480490","480495","480492","480491","480493","480494","480486","480487","480489"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Revitalization of the NAL two-dimensional transonic wind tunnel: Renewal of the wind tunnel in the relation to control system"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1999-05","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"55","bibliographicPageStart":"45","bibliographicVolumeNumber":"42","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所特別資料"},{"bibliographic_title":"Special Publication of National Aerospace Laboratory","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":"21-22 May 1998 (60th). 26-27 Nov. 1998 (61st)","subitem_description_type":"Other"}]},"item_5_description_15":{"attribute_name":"会議概要（会議名, 開催地, 会期, 主催者等）（英）","attribute_value_mlt":[{"subitem_description":"21-22 May 1998 (60th). 26-27 Nov. 1998 (61st)","subitem_description_type":"Other"}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"航技研2次元風洞の改修工事終了に伴い風洞の特徴について報告する。測定部を大型化することによって模型付近の流れに及ぼす側壁の影響が軽減化された上、作業性(安全性)が向上し、また従来の2次元翼型試験に加えスティング・ストラット方式による3次元模型試験が可能となった。さらに可変ノズルを新設することでマッハ数領域を1.4まで拡張した。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"This is the report on the features of the revitalized National Aerospace Laboratory (NAL) two dimensional transonic wind tunnel. With the enlargement of the test section, the effect of the walls on the flow near the model is reduced, the efficiency (the safety) is improved, and three dimensional model tests by sting strut mode are now possible as well as the conventional two dimensional airfoil tests. Further, the Mach number range is expanded to 1.4 with the newly installed variable nozzle.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0001959006","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: NAL SP-42","subitem_description_type":"Other"}]},"item_5_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"航空宇宙技術研究所"}]},"item_5_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"National Aerospace Laboratory (NAL)"}]},"item_5_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0289-260X","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":"AN10097345","subitem_source_identifier_type":"NCID"}]},"item_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"航空宇宙技術研究所 空力特性研究部　二次元風洞研究室"},{"subitem_text_value":"航空宇宙技術研究所 空力特性研究部　二次元風洞研究室"},{"subitem_text_value":"航空宇宙技術研究所 空力特性研究部　二次元風洞研究室"},{"subitem_text_value":"航空宇宙技術研究所 空力特性研究部　二次元風洞研究室"},{"subitem_text_value":"航空宇宙技術研究所 空力特性研究部　二次元風洞研究室"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Two-Dimensional Wind Tunnel Laboratory, Aerodynamics Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Two-Dimensional Wind Tunnel Laboratory, Aerodynamics Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Two-Dimensional Wind Tunnel Laboratory, Aerodynamics Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Two-Dimensional Wind Tunnel Laboratory, Aerodynamics Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Two-Dimensional Wind Tunnel Laboratory, Aerodynamics Division"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"佐藤, 衛"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"神田, 宏"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"須谷, 記和"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"重見, 仁"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"戸田, 亘洋"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Sato, Mamoru","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kanda, Hiroshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Sudani, Norikazu","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Shigemi, Masashi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Toda, Nobuhiro","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":"2020-02-10"}],"displaytype":"detail","filename":"nalsp0042006.pdf","filesize":[{"value":"1.1 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0042006.pdf","url":"https://jaxa.repo.nii.ac.jp/record/37386/files/nalsp0042006.pdf"},"version_id":"505665ef-3e9f-4f04-96b5-b485c229fe8b"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"2次元風洞","subitem_subject_scheme":"Other"},{"subitem_subject":"スティング・ストラット方式","subitem_subject_scheme":"Other"},{"subitem_subject":"3次元模型試験","subitem_subject_scheme":"Other"},{"subitem_subject":"2次元翼型試験","subitem_subject_scheme":"Other"},{"subitem_subject":"可変ノズル","subitem_subject_scheme":"Other"},{"subitem_subject":"マッハ数","subitem_subject_scheme":"Other"},{"subitem_subject":"安全性","subitem_subject_scheme":"Other"},{"subitem_subject":"作業性","subitem_subject_scheme":"Other"},{"subitem_subject":"サウンドサプレッサ","subitem_subject_scheme":"Other"},{"subitem_subject":"側壁境界層","subitem_subject_scheme":"Other"},{"subitem_subject":"多穴板","subitem_subject_scheme":"Other"},{"subitem_subject":"抽気フラップ","subitem_subject_scheme":"Other"},{"subitem_subject":"two dimensional transonic wind tunnel","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"sting strut mode","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"three dimensional model test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"two dimensional airfoil test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"variable nozzle","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Mach number","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"safety","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"efficiency","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"sound suppressor","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"side wall boundary layer","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"porus board","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"bleeding flap","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 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