{"created":"2023-06-20T15:13:17.037519+00:00","id":43210,"links":{},"metadata":{"_buckets":{"deposit":"44e61769-8098-40e2-9468-cda6c0bff412"},"_deposit":{"created_by":1,"id":"43210","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"43210"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00043210","sets":["1887:1893","1896:1898:1913:1915"]},"author_link":["462633","462639","462635","462637","462634","462632","462636","462638"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Investigation of a Prediction Method of Transonic Flutter Characteristics Using Unsteady Transonic Aerodynamics"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1985-11","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"250","bibliographicPageStart":"243","bibliographicVolumeNumber":"5","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-5","bibliographic_titleLang":"en"}]}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"In this paper, theoretical studies to predict aircraft transonic flutter phenomena are reviewed and a new practical method based on nonlinear transonic aerodynamics is proposed for estimating flutter characteristics of aircraft in their initial design phase. This analytical tool consists of two and three dimensional subsonic aerodynamic calculation corrected by two-dimensional transonic aerodynamic computations to account for the shock movement on the wing surface. The present analytical procedure is fairly good at predicting the flutter characteristics of the wing wind tunnel flutter test model of the YXX, the next commercial transport currently under study. This result indicates the wide applicability of the method to the flutter estimation of aircraft with high aspect ratio wings.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALSP0005030","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-5","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":"三菱重工業株式会社"},{"subitem_text_value":"三菱重工業株式会社"},{"subitem_text_value":"三菱重工業株式会社"},{"subitem_text_value":"財団法人日本航空機開発協会"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"荒川, 治彦"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"野本, 秀喜"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"戸田, 信雄"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"平岡, 康一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Arakawa, Haruhiko","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nomoto, Hideki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Toda, Nobuo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hiraoka, Kouichi","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":"nalsp0005030.pdf","filesize":[{"value":"556.0 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0005030.pdf","url":"https://jaxa.repo.nii.ac.jp/record/43210/files/nalsp0005030.pdf"},"version_id":"cca5e9c6-6f4f-4ae0-9033-264ebcd8e2f9"}]},"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":"非定常遷音速空気力計算法を用いたフラッタ解析法","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"非定常遷音速空気力計算法を用いたフラッタ解析法"}]},"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":"43210","relation_version_is_last":true,"title":["非定常遷音速空気力計算法を用いたフラッタ解析法"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T22:20:13.923809+00:00"}