{"created":"2023-06-20T15:07:05.294846+00:00","id":36468,"links":{},"metadata":{"_buckets":{"deposit":"d5428186-d89e-4eb1-9eee-6ee54403be19"},"_deposit":{"created_by":1,"id":"36468","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"36468"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00036468","sets":["1887:1890","1896:1898:1899:1906"]},"author_link":["423785","423788","423786","423787"],"item_9_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1937-07","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"384","bibliographicPageStart":"375","bibliographicVolumeNumber":"155","bibliographic_titles":[{"bibliographic_title":"東京帝國大學航空研究所彙報"}]}]},"item_9_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"A small four-bladed wind vane was placed behind a wing model, and the rate of rotation was measured stroboscopically in order to investigate the lift distribution along the span. It was found both theoretically and experimentally that the rate of rotation was nearly proportional to dГ/dy, where Гis the circulation and y is the distance along the span, provided that the wind vane was sufficiently small and properly placed behind the model. The allowable diameter of the wind vane is estimated to be of the order of one per cent of the span. The present miniature test was made as a preliminary investigation in order to determine the applicablity of a wind vane for such a purpose. It is hoped in the near future to make the test in the larger scale.","subitem_description_type":"Other"}]},"item_9_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: SA4433720000","subitem_description_type":"Other"}]},"item_9_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"東京帝國大學航空研究所"}]},"item_9_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AN00162779","subitem_source_identifier_type":"NCID"}]},"item_9_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"航空學教室"},{"subitem_text_value":"航空學科"},{"subitem_text_value":"飛行機部:(現)柳製作所"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"谷, 一郎"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"花田, 實"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"森口, 繁一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"清水, 惣治"}],"nameIdentifiers":[{}]}]},"item_files":{"attribute_name":"ファイル情報","attribute_type":"file","attribute_value_mlt":[{"accessrole":"open_date","date":[{"dateType":"Available","dateValue":"2020-01-24"}],"displaytype":"detail","filename":"SA4433720.pdf","filesize":[{"value":"718.1 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"SA4433720.pdf","url":"https://jaxa.repo.nii.ac.jp/record/36468/files/SA4433720.pdf"},"version_id":"e53301c0-9ba2-488e-8642-4ed9df42ab7b"}]},"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":"風車を用ひて翼幅に沿ふ揚力分布を測定する試み","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"風車を用ひて翼幅に沿ふ揚力分布を測定する試み"}]},"item_type_id":"9","owner":"1","path":["1890","1906"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"36468","relation_version_is_last":true,"title":["風車を用ひて翼幅に沿ふ揚力分布を測定する試み"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T22:56:10.541622+00:00"}