{"created":"2023-06-20T15:02:24.155755+00:00","id":31491,"links":{},"metadata":{"_buckets":{"deposit":"81cfbe0e-222d-4013-9c4d-c6d2eca51611"},"_deposit":{"created_by":1,"id":"31491","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"31491"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00031491","sets":["1887:1890","1896:1898:1899:1910"]},"author_link":["404480","404479","404484","404481","404483","404482"],"item_9_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"New Transonic, Oscillatfng-aerofoil Wind Tunnel"}]},"item_9_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1974-06","bibliographicIssueDateType":"Issued"},"bibliographicIssueNumber":"2_B","bibliographicPageEnd":"285","bibliographicPageStart":"271","bibliographicVolumeNumber":"10","bibliographic_titles":[{"bibliographic_title":"東京大学宇宙航空研究所報告"}]}]},"item_9_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"本報告は新設の巡音速振動具風洞の構造と特性について述べたものである。遷音速振動翼風洞は,平行使をもつ二次元旅路中で振動する翼の遷音速特性を明らかにすることを目的として設計製作されたものであって,測定部には上下固定壁の内側に二枚の可動壁を持ち,測定部流路の高さを任意に変え得ることを特徴としている.供試翼には特殊な加振機構により振り振動が与えられ,振動具に作用する空気力を測定するとともに,反射光式シュリーレン装仮により流れの光学的可視観察を行うことができる.選音速振動翼風洞の主な仕様は次の通りである.","subitem_description_type":"Abstract"}]},"item_9_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"This paper gives the construction and characteristics of a new transonic wind tunnel which was designed and constructed for the experiments concerning a oscillating aerofoil in transonic channel flow. This wind tunnel is characterized by the test section of variable height, which is furnished with two movable parallel walls placed between upper and lower rigid walls of the wind tunnel. Test aerofoil is given a forced torsional oscillation, and measurements of the oscillatory aerodynamic forces acting on the aerofoil are made as well as the flow visualization with the schlieren method of reflex type. The specifications of the transonic wind tunnel are as follows: Wind tunnel: Type:blow-down type Test section:width 75mm, maximum height 200mm (variable) Mach number:equal to or less than 1.0 Running time:over 15min. Aerofoil oscillation mechanism: Type:forced torsional oscillation by two electro-magnetic oscillators (with resonance method) Maximum force of oscillation: 150kg × 2 Frequency of oscillation:5～2,000Hz","subitem_description_type":"Other"}]},"item_9_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: SA0124388000","subitem_description_type":"Other"}]},"item_9_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"東京大学宇宙航空研究所"}]},"item_9_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0563-8100","subitem_source_identifier_type":"ISSN"}]},"item_9_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AN00161914","subitem_source_identifier_type":"NCID"}]},"item_9_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"東京大学宇宙航空研究所"},{"subitem_text_value":"東京大学宇宙航空研究所"},{"subitem_text_value":"東京大学院工学系研究科"}]},"item_9_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Institute of Space and Aeroautical Science University of Tokyo"},{"subitem_text_language":"en","subitem_text_value":"Institute of Space and Aeroautical Science University of Tokyo"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"谷田, 奸通"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"浅沼, 強"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"斎藤, 喜夫"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"TANIDA, Yoshimichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"ASANUMA, Tsuyoshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"SAITO, Yoshio","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":"2020-01-23"}],"displaytype":"detail","filename":"SA0124388.pdf","filesize":[{"value":"1.6 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"SA0124388.pdf","url":"https://jaxa.repo.nii.ac.jp/record/31491/files/SA0124388.pdf"},"version_id":"9dac26cd-2efc-455e-8fcd-be42a5f313b2"}]},"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":"departmental bulletin paper","resourceuri":"http://purl.org/coar/resource_type/c_6501"}]},"item_title":"遷音速振動翼風洞","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"遷音速振動翼風洞"}]},"item_type_id":"9","owner":"1","path":["1890","1910"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"31491","relation_version_is_last":true,"title":["遷音速振動翼風洞"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T00:58:29.454713+00:00"}