{"created":"2023-06-20T15:13:20.357262+00:00","id":43266,"links":{},"metadata":{"_buckets":{"deposit":"acfbd950-8754-4380-bf84-e7bbc37d7ee0"},"_deposit":{"created_by":1,"id":"43266","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"43266"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00043266","sets":["1887:1893","1896:1898:1913:1915"]},"author_link":["462928","462929","462925","462927","462930","462926"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Calculations of Unsteady Aerodynamics for a Full Aircraft Configuration Using Boundary Element Method"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1987-11","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"102","bibliographicPageStart":"91","bibliographicVolumeNumber":"8","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所特別資料"},{"bibliographic_title":"Special Publication of National Aerospace Laboratory SP-8","bibliographic_titleLang":"en"}]}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"A boundary element method is presented for determining aerodynamic loadings on arbitrary configurations in oscillatory subsonic flow. Formulas (modified Morino's method) are given for the unsteady pressure distributions or unsteady force experienced in subsonic flow by the wing-store combination, oscillating in the torsional oscillations about a fixed axis parallel to the span and other oscillating modes (flapping, plunging). Interference effects from an underwing pylon store were analyzed. The method is finally verified through comparison with experiment for the model at angles of attack from -5 degree to +5 degree, and reduced frequencies from 0.65 to l.3 at low subsonic flow.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALSP0008013","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 SP-8","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":"0289-260X","subitem_source_identifier_type":"ISSN"}]},"item_3_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AN10097345","subitem_source_identifier_type":"NCID"}]},"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"},{"subitem_text_value":"航空宇宙技術研究所"},{"subitem_text_value":"三菱重工業株式会社名古屋航空機製作所"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"},{"subitem_text_language":"en","subitem_text_value":"Mitsubishi Heavy Industries Ltd."}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"柳沢, 三憲"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"森田, 甫之"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"巽, 重文"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yanagizawa, Mitsunori","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Morita, Toshiyuki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Tatsumi, Shigefumi","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":"2020-01-28"}],"displaytype":"detail","filename":"nalsp0008013.pdf","filesize":[{"value":"702.3 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0008013.pdf","url":"https://jaxa.repo.nii.ac.jp/record/43266/files/nalsp0008013.pdf"},"version_id":"88fe8158-551c-4a7a-84ea-75cc1af32e7c"}]},"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":"technical report","resourceuri":"http://purl.org/coar/resource_type/c_18gh"}]},"item_title":"境界要素法による全機形態の非定常空力計算","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"境界要素法による全機形態の非定常空力計算"}]},"item_type_id":"3","owner":"1","path":["1893","1915"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"43266","relation_version_is_last":true,"title":["境界要素法による全機形態の非定常空力計算"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T22:18:54.354785+00:00"}