{"created":"2023-06-20T15:06:00.099810+00:00","id":35391,"links":{},"metadata":{"_buckets":{"deposit":"8d857bd8-77f1-4e4e-9bcb-0d17ae291d61"},"_deposit":{"created_by":1,"id":"35391","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"35391"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00035391","sets":["1887:1890","1896:1898:1899:1993"]},"author_link":["421870","421871"],"item_9_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"On the Velocity Distribution round an Aerofoil at High Speeds, I."}]},"item_9_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1944-04","bibliographicIssueDateType":"Issued"},"bibliographicIssueNumber":"290","bibliographicPageEnd":"202","bibliographicPageStart":"147","bibliographicVolumeNumber":"21","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":"§12. On the basis of a new method of M^2-expansion, analytical formulae are obtained, which give the velocity distribution on an arbitrary wing section placed in a uniform flow of a compressible fluid exactly to the order of M^4, M being the MACH number of the undisturbed stream. These formulae would be of particular value for the purely numerical work, though in some cases they will also enable us to find analytical expressions for the velocity distribution. Examples of the application of the formulae, both analytical and numerical, will be given in forthcoming papers.","subitem_description_type":"Other"}]},"item_9_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: SA4146851000","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":"今井, 功"}],"nameIdentifiers":[{"nameIdentifier":"421870","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"IMAI, Isao","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"421871","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":"SA4146851.pdf","filesize":[{"value":"2.5 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"SA4146851.pdf","url":"https://jaxa.repo.nii.ac.jp/record/35391/files/SA4146851.pdf"},"version_id":"cd12971f-a94a-4f65-be1b-62e32e20cd66"}]},"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":"高速度における翼型のまはりの速度分布について,II.圓柱及び圓弧翼","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"高速度における翼型のまはりの速度分布について,II.圓柱及び圓弧翼"}]},"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":"35391","relation_version_is_last":true,"title":["高速度における翼型のまはりの速度分布について,II.圓柱及び圓弧翼"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T23:20:32.687762+00:00"}