{"created":"2023-06-20T15:07:49.513885+00:00","id":37188,"links":{},"metadata":{"_buckets":{"deposit":"0a02e663-32d4-4f27-9e11-77cb1da7a79e"},"_deposit":{"created_by":1,"id":"37188","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"37188"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00037188","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["479409","479413","479412","479406","479407","479408","479411","479410"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Revitalization of NAL transonic two-dimensional wind tunnel"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1998-01","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"66","bibliographicPageStart":"57","bibliographicVolumeNumber":"38","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":"22-23 May 1997 (58th). 27-28 Nov. 1997 (59th)","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":"22-23 May 1997 (58th). 27-28 Nov. 1997 (59th)","subitem_description_type":"Other"}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"航空宇宙技術研究所2次元風洞は1979年に竣工し、実機相当のレイノルズ数を実現できる風洞として、多くの試験に用いられてきた。しかし近年老朽化が進み試験の実施に支障を来すことが多くなった。そこで1995年度から改修に取り掛かり、近く完成する見通しである。新しい2次元風洞では老朽化に対する処置に加えて、測定部の大きさの変更、可変ノズルの導入などを盛り込み、可能な試験の範囲を拡張すると同時に、作業性の向上、データの高精度化を図った。本報告は新しい2次元風洞の概要について述べる。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The NAL transonic two-dimensional wind tunnel was constructed in 1979, and has been used as a facility, in which tests can be realized under the condition of Reynolds number equivalent to that of an aircraft. However, it became so superannuated recently as difficult to carry out tests without trouble. Hence revitalization of the facility was started in 1995, and it will be completed at an early date. For the renewed two-dimensional wind tunnel, the improvement of operational function and data accuracy were attempted, simultaneously with expanding the possible test range by incorporating such renewal as making measuring part large-scaled and introducing a variable nozzle, in addition to the treatment for superannuating. This paper outlines the renewed two-dimensional wind tunnel.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0001434006","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-38","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"},{"subitem_text_value":"航空宇宙技術研究所"},{"subitem_text_value":"航空宇宙技術研究所"},{"subitem_text_value":"航空宇宙技術研究所"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"重見, 仁"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"神田, 宏"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"佐藤, 衛"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"須谷, 記和"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Shigemi, Masashi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kanda, Hiroshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Sato, Mamoru","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Sudani, Norikazu","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":"nalsp0038006.pdf","filesize":[{"value":"778.0 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0038006.pdf","url":"https://jaxa.repo.nii.ac.jp/record/37188/files/nalsp0038006.pdf"},"version_id":"b7d37cff-62ee-49b7-8134-591c6cbfe2a4"}]},"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":"高レイノルズ数風洞試験","subitem_subject_scheme":"Other"},{"subitem_subject":"風洞改修","subitem_subject_scheme":"Other"},{"subitem_subject":"風洞制御装置","subitem_subject_scheme":"Other"},{"subitem_subject":"風洞計測システム","subitem_subject_scheme":"Other"},{"subitem_subject":"可変ノズル","subitem_subject_scheme":"Other"},{"subitem_subject":"風洞測定部","subitem_subject_scheme":"Other"},{"subitem_subject":"気流整流装置","subitem_subject_scheme":"Other"},{"subitem_subject":"two dimensional wind tunnel","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"high Reynolds number wind tunnel test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wind tunnel revitalization","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wind tunnel control system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wind tunnel measurement system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"variable nozzle","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wind tunnel measurement part","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"air flow straightening device","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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