{"created":"2023-06-20T15:15:06.852845+00:00","id":45169,"links":{},"metadata":{"_buckets":{"deposit":"ec75c615-f07e-4bd4-b0d1-48ae35bdf5f1"},"_deposit":{"created_by":1,"id":"45169","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"45169"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00045169","sets":["1887:1893","1896:1898:1913:1917"]},"author_link":["473264","473265","473260","473266","473261","473262","473263","473267"],"item_3_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"航技研0.1m×0.1m遷音速低温風洞の試作"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1986-08","bibliographicIssueDateType":"Issued"},"bibliographicPageStart":"57","bibliographicVolumeNumber":"910","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所報告"},{"bibliographic_title":"Technical Report of National Aerospace Laboratory TR-910","bibliographic_titleLang":"en"}]}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"In order to study the cryogenic wind tunnel, in which high Reynolds number tests can be conducted, a small transonic cryogenic wind tunnel was constructed. The construction and the operational results are described in this paper. This small cryogenic wind tunnel, with a test section of 0.1m×0.1m, was built to ascertain the basic design specifications for a large transonic cryogenic wind tunnel which will be constructed in the future, and also to gain skill in operating the cryogenic wind tunnel. The capability of this wind tunnel is from stagnation temperature down to -173C, for Mach numbers ranging from 0.4 to 1.02 and for a unit Reynolds number up to 1.3×10(exp 6)/cm with more than one hour running time. In this paper, the design concept is first briefly given, then, the complete system i.e. the wind tunnel, the liquid nitrogen supply system, the gas nitrogen exhaust system, the thermal insulation device, the fan and the drive motor and the instrumentation and operating system, are described in detail. Finally, the experimental results are discussed. The conclusion is that cryogenic wind tunnel operation can be safely and successfully conducted.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALTR0910000","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: NAL TR-910","subitem_description_type":"Other"}]},"item_3_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"航空宇宙技術研究所"}]},"item_3_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"National Aerospace Laboratory(NAL)"}]},"item_3_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0389-4010","subitem_source_identifier_type":"ISSN"}]},"item_3_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"航空宇宙技術研究所空気力学第二部"},{"subitem_text_value":"航空宇宙技術研究所空気力学第二部"},{"subitem_text_value":"航空宇宙技術研究所空気力学第二部"},{"subitem_text_value":"航空宇宙技術研究所空気力学第二部"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Second Aerodynamics Division, National Aerospace Laboratory(NAL)"},{"subitem_text_language":"en","subitem_text_value":"Second Aerodynamics Division, National Aerospace Laboratory(NAL)"},{"subitem_text_language":"en","subitem_text_value":"Second Aerodynamics Division, National Aerospace Laboratory(NAL)"},{"subitem_text_language":"en","subitem_text_value":"Second Aerodynamics Division, National Aerospace Laboratory(NAL)"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"高島, 一明"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"沢田, 秀夫"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"青木, 竹夫"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"萱場, 重男"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"TAKASHIMA, Kazuaki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"SAWADA, Hideo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"AOKI, Takeo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"KAYABA, Shigeo","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":"2020-01-29"}],"displaytype":"detail","filename":"naltr00910.pdf","filesize":[{"value":"4.5 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltr00910.pdf","url":"https://jaxa.repo.nii.ac.jp/record/45169/files/naltr00910.pdf"},"version_id":"42c4029d-cbed-43d9-85ea-6cc89183e112"}]},"item_language":{"attribute_name":"言語","attribute_value_mlt":[{"subitem_language":"eng"}]},"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":"Trial Manufacture of NAL 0.1m×0.1m Transonic Cryogenic Wind Tunnel","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Trial Manufacture of NAL 0.1m×0.1m Transonic Cryogenic Wind Tunnel","subitem_title_language":"en"}]},"item_type_id":"3","owner":"1","path":["1893","1917"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"45169","relation_version_is_last":true,"title":["Trial Manufacture of NAL 0.1m×0.1m Transonic Cryogenic Wind Tunnel"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:44:07.899448+00:00"}