{"created":"2023-06-20T15:15:08.419640+00:00","id":45196,"links":{},"metadata":{"_buckets":{"deposit":"4652aa31-e346-4cfa-93d1-803d114b70ba"},"_deposit":{"created_by":1,"id":"45196","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"45196"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00045196","sets":["1887:1893","1896:1898:1913:1917"]},"author_link":["473412","473411"],"item_3_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"亜音速流中で振動する翼およびプロペラの理論における無限遠の条件"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1987-07","bibliographicIssueDateType":"Issued"},"bibliographicPageStart":"8","bibliographicVolumeNumber":"937","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所報告"},{"bibliographic_title":"Technical Report of National Aerospace Laboratory TR-937","bibliographic_titleLang":"en"}]}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Conditions at infinity that should be satisfied by the acceleration potential of the flow field around oscillating wings or propellers in a uniform subsonic flow are given in simple forms. It is shown that the value of the integral on the boundary surface at infinity in Green’s formula becomes zero by virtue of these conditions, if, in addition, reasonable conditions at infinity are assigned for the fundamental solution of the adjoint equation of the governing differential equation.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALTR0937000","subitem_description_type":"Other"}]},"item_3_description_33":{"attribute_name":"レポート番号","attribute_value_mlt":[{"subitem_description":"レポート番号: NAL TR-937","subitem_description_type":"Other"}]},"item_3_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"航空宇宙技術研究所"}]},"item_3_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"National Aerospace Laboratory(NAL)"}]},"item_3_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0389-4010","subitem_source_identifier_type":"ISSN"}]},"item_3_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"航空宇宙技術研究所機体第一部"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"First Airframe Division, National Aerospace Laboratory(NAL)"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"市川, 輝雄"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"ICHIKAWA, Teruo","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":"2020-01-29"}],"displaytype":"detail","filename":"naltr00937.pdf","filesize":[{"value":"533.2 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltr00937.pdf","url":"https://jaxa.repo.nii.ac.jp/record/45196/files/naltr00937.pdf"},"version_id":"bdbb3589-6640-4dd5-979e-359335f455b8"}]},"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":"technical report","resourceuri":"http://purl.org/coar/resource_type/c_18gh"}]},"item_title":"Conditions at Infinity for Theories of Oscillating Wings and Propellers in Subsonic Flow","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Conditions at Infinity for Theories of Oscillating Wings and Propellers in Subsonic Flow","subitem_title_language":"en"}]},"item_type_id":"3","owner":"1","path":["1893","1917"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"45196","relation_version_is_last":true,"title":["Conditions at Infinity for Theories of Oscillating Wings and Propellers in Subsonic Flow"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:43:35.809596+00:00"}