{"created":"2023-06-20T15:06:05.648374+00:00","id":35501,"links":{},"metadata":{"_buckets":{"deposit":"6512b34e-c86b-4110-a19b-27a361c9a196"},"_deposit":{"created_by":1,"id":"35501","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"35501"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00035501","sets":["1887:1890","1896:1898:1899:1993"]},"author_link":["422223"],"item_9_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1932-11","bibliographicIssueDateType":"Issued"},"bibliographicIssueNumber":"88","bibliographicPageEnd":"194","bibliographicPageStart":"179","bibliographicVolumeNumber":"7","bibliographic_titles":[{"bibliographic_title":"東京帝國大學航空研究所報告"},{"bibliographic_title":"Report of Aeronautical Research Institute, Tokyo Imperial University","bibliographic_titleLang":"en"}]}]},"item_9_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"In present-day practice an aeroplane can be designed with confidence as to performance, strength, and stability upon data supplied by theoretical analysis. But in the design of control surfaces there is an element of risk in that the designer has only his own experience and the judgement of test-pilots to rely on. In this paper the constant initial angular acceleration is calculated for an aeroplane flying with minimum velocity, and rolling soon after the aileron has been suddenly actuated (angular velocity 1 rad./sec.). The conclusion is that control surfaces should be so designed that the angular acceleration shall be greater than the mean value of the angular acceleration for that class in which the aeroplane belongs.","subitem_description_type":"Other"}]},"item_9_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: SA4148264000","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_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Aeronautical Research Institute, Tokyo Imperial University"}]},"item_9_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AA00387631","subitem_source_identifier_type":"NCID"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"OGAWA, Taitiro","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"422223","nameIdentifierScheme":"WEKO"}]}]},"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":"SA4148264.pdf","filesize":[{"value":"649.2 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"SA4148264.pdf","url":"https://jaxa.repo.nii.ac.jp/record/35501/files/SA4148264.pdf"},"version_id":"859260db-7229-40f9-80d6-a7bf7bff56cf"}]},"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":"departmental bulletin paper","resourceuri":"http://purl.org/coar/resource_type/c_6501"}]},"item_title":"A Design Formula for Ailerons.","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"A Design Formula for Ailerons.","subitem_title_language":"en"}]},"item_type_id":"9","owner":"1","path":["1890","1993"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"35501","relation_version_is_last":true,"title":["A Design Formula for Ailerons."],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T23:18:18.707095+00:00"}