{"created":"2021-03-01T06:18:59.639663+00:00","id":12060,"links":{},"metadata":{"_buckets":{"deposit":"3df0ce11-eddd-48a4-951c-7b0fc6410ad4"},"_deposit":{"id":"12060","owners":[],"pid":{"revision_id":0,"type":"depid","value":"12060"},"status":"published"},"_oai":{"id":"oai:nagoya.repo.nii.ac.jp:00012060","sets":["320:321:322"]},"author_link":["38248","38249","38250","38251","38252","38253","38254","38255","38256","38257"],"item_10_alternative_title_19":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"Flutter Analysis of a Curved PanelUsing a Fluid-Structure Coupled Scheme","subitem_alternative_title_language":"en"}]},"item_10_biblio_info_6":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2007","bibliographicIssueDateType":"Issued"},"bibliographicIssueNumber":"638","bibliographicPageEnd":"155","bibliographicPageStart":"150","bibliographicVolumeNumber":"55","bibliographic_titles":[{"bibliographic_title":"日本航空宇宙学会論文集","bibliographic_titleLang":"ja"}]}]},"item_10_description_4":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"A computational program using a CFD-CSD coupled method has been developed to study the problem of low supersonic curved panel flutter. So far the supersonic aerodynamic model has been commonly employed to compute flutter boundaries. However, the present CFD-CSD coupled method makes it possible to analyze flutter boundaries at all speeds including transonic speeds. The computed flutter dynamic pressure for M∞=3 agrees with others’ results. A curved panel flutter were analyzed at a low supersonic speed, M∞=1.2. The flutter for small curvature panels is first-mode flutter, which is similar to flat panel flutter, whereas it becomes higher-mode flutter for larger curvature plates. In this study, flutter boundaries for an access panel have also been simulated. Its critical dynamic pressure becomes significantly lower compared with the case of a panel with its all edges simply supported.","subitem_description_language":"en","subitem_description_type":"Abstract"}]},"item_10_identifier_60":{"attribute_name":"URI","attribute_value_mlt":[{"subitem_identifier_type":"HDL","subitem_identifier_uri":"http://hdl.handle.net/2237/13938"}]},"item_10_publisher_32":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"日本航空宇宙学会","subitem_publisher_language":"ja"}]},"item_10_select_15":{"attribute_name":"著者版フラグ","attribute_value_mlt":[{"subitem_select_item":"publisher"}]},"item_10_source_id_7":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"1344-6460","subitem_source_identifier_type":"PISSN"}]},"item_10_text_14":{"attribute_name":"フォーマット","attribute_value_mlt":[{"subitem_text_value":"application/pdf"}]},"item_1615787544753":{"attribute_name":"出版タイプ","attribute_value_mlt":[{"subitem_version_resource":"http://purl.org/coar/version/c_970fb48d4fbd8a85","subitem_version_type":"VoR"}]},"item_access_right":{"attribute_name":"アクセス権","attribute_value_mlt":[{"subitem_access_right":"open access","subitem_access_right_uri":"http://purl.org/coar/access_right/c_abf2"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"橋本, 敦","creatorNameLang":"ja"}],"nameIdentifiers":[{"nameIdentifier":"38248","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Hashimoto, Atsushi","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"38249","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"八木, 直人","creatorNameLang":"ja"}],"nameIdentifiers":[{"nameIdentifier":"38250","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Yagi, Naoto","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"38251","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"中村, 佳朗","creatorNameLang":"ja"}],"nameIdentifiers":[{"nameIdentifier":"38252","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Nakamura, Yoshiaki","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"38253","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"伊藤, 文博","creatorNameLang":"ja"}],"nameIdentifiers":[{"nameIdentifier":"38254","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Ito, Fumihiro","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"38255","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"海田, 武司","creatorNameLang":"ja"}],"nameIdentifiers":[{"nameIdentifier":"38256","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Kaiden, Takeshi","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"38257","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":"2018-02-20"}],"displaytype":"detail","filename":"jjsass_v55_n638.pdf","filesize":[{"value":"1.0 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"jjsass_v55_n638.pdf","objectType":"fulltext","url":"https://nagoya.repo.nii.ac.jp/record/12060/files/jjsass_v55_n638.pdf"},"version_id":"74a9e722-6821-4b1a-9a50-daa0f9ef0016"}]},"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":"journal article","resourceuri":"http://purl.org/coar/resource_type/c_6501"}]},"item_title":"曲面パネルの流体構造連成計算法によるフラッタ解析","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"曲面パネルの流体構造連成計算法によるフラッタ解析","subitem_title_language":"ja"}]},"item_type_id":"10","owner":"1","path":["322"],"pubdate":{"attribute_name":"PubDate","attribute_value":"2010-08-03"},"publish_date":"2010-08-03","publish_status":"0","recid":"12060","relation_version_is_last":true,"title":["曲面パネルの流体構造連成計算法によるフラッタ解析"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-01-16T03:58:44.435097+00:00"}