{"created":"2023-06-20T15:03:24.615176+00:00","id":32613,"links":{},"metadata":{"_buckets":{"deposit":"8f8dc3d9-994f-4e3f-bc90-d45e2c33ec39"},"_deposit":{"created_by":1,"id":"32613","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"32613"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00032613","sets":["1887:1890","1896:1898:1899:1910"]},"author_link":["410367","410368","410369","410370"],"item_9_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Aerofoil Response in Oblique Gust"}]},"item_9_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1981-02","bibliographicIssueDateType":"Issued"},"bibliographicIssueNumber":"1_A","bibliographicPageEnd":"34","bibliographicPageStart":"23","bibliographicVolumeNumber":"17","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":"Searsによる翼のガスト応答の問題を,亜音速流れ中でexp[iω(t-x/V)+iλz]と表わされる3次元的ガストに拡張し,特異点法を用いて解いた.翼の前縁に対してガスト波面が傾斜する効果が大きいことが結論された.","subitem_description_type":"Abstract"}]},"item_9_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The Sears type lift functions (Imaginery vs. real parts of the unsteady lift coefficient) of an aerofoil operating in sinusoidal gusts of a general form: exp[iω (t-x/V) + iλz)] with a subsonic flow have been calculated. The obliqueness of the gust wave front with respect to the aerofoil leading edge is found to be very influencial upon the aerodynamic lift and moment.","subitem_description_type":"Other"}]},"item_9_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: SA0125949000","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"}]},"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 Aeronautical Science, University of Tokyo"},{"subitem_text_language":"en","subitem_text_value":"Institute of Space and Aeronautical Science, University of Tokyo"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"長島, 利夫"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"谷田, 好通"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"NAGASHIMA, Toshio","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"TANIDA, Yoshimichi","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":"2020-01-24"}],"displaytype":"detail","filename":"SA0125949.pdf","filesize":[{"value":"389.4 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"SA0125949.pdf","url":"https://jaxa.repo.nii.ac.jp/record/32613/files/SA0125949.pdf"},"version_id":"457b5c80-4f82-4317-8505-ceb43c1ea510"}]},"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":"<論文>圧縮流れ中の翼のガスト応答と傾斜効果","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"<論文>圧縮流れ中の翼のガスト応答と傾斜効果"}]},"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":"32613","relation_version_is_last":true,"title":["<論文>圧縮流れ中の翼のガスト応答と傾斜効果"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T00:27:59.443029+00:00"}