{"created":"2023-06-20T14:38:59.984299+00:00","id":5662,"links":{},"metadata":{"_buckets":{"deposit":"2905735a-5e14-4f13-bc7d-cad53d9819c8"},"_deposit":{"created_by":1,"id":"5662","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"5662"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00005662","sets":["1887:1891","9:789:972:991"]},"author_link":["27767"],"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2008-02-29","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"76","bibliographicPageStart":"64","bibliographicVolumeNumber":"JAXA-SP-07-008E","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構特別資料"},{"bibliographic_title":"JAXA Special Publication: Proceedings of Lectures and Workshop International: Recent Advances in Multidisciplinary Technology and Modeling","bibliographic_titleLang":"en"}]}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Using full continuum models, we establish purely theoretically that in two-dimensional isentropic flow, the flutter speed for a slender high-aspect ratio wing is a Hopf bifurcation point of the aeroelastic structure dynamics which can be expressed as a non-linear convolution evolution equation. The flutter speed is determined by the linearized model and the LCO (Limit Cycle Oscillation) is periodic with period (2 pi/omega) where omega is the angular flutter frequency in the linear model, and can be expressed as a harmonic series.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0063824007","subitem_description_type":"Other"}]},"item_5_description_33":{"attribute_name":"レポート番号","attribute_value_mlt":[{"subitem_description":"レポート番号: JAXA-SP-07-008E","subitem_description_type":"Other"}]},"item_5_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙航空研究開発機構"}]},"item_5_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Japan Aerospace Exploration Agency (JAXA)"}]},"item_5_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"1349-113X","subitem_source_identifier_type":"ISSN"}]},"item_5_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AA11984031","subitem_source_identifier_type":"NCID"}]},"item_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"University of California, Los Angeles Flight Systems Research Center"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"University of California, Los Angeles Flight Systems Research Center"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"Balakrishnan, A. V.","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":"2020-01-16"}],"displaytype":"detail","filename":"63824007.pdf","filesize":[{"value":"399.7 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"63824007.pdf","url":"https://jaxa.repo.nii.ac.jp/record/5662/files/63824007.pdf"},"version_id":"6be2a5be-2993-4da4-a4b4-cc288c440f49"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"2次元流","subitem_subject_scheme":"Other"},{"subitem_subject":"フラッタ","subitem_subject_scheme":"Other"},{"subitem_subject":"フラッタ解析","subitem_subject_scheme":"Other"},{"subitem_subject":"等エントロピー流","subitem_subject_scheme":"Other"},{"subitem_subject":"高アスペクト比翼","subitem_subject_scheme":"Other"},{"subitem_subject":"空力弾性","subitem_subject_scheme":"Other"},{"subitem_subject":"航空機設計","subitem_subject_scheme":"Other"},{"subitem_subject":"航空機構造","subitem_subject_scheme":"Other"},{"subitem_subject":"翼振動","subitem_subject_scheme":"Other"},{"subitem_subject":"リミットサイクル振動","subitem_subject_scheme":"Other"},{"subitem_subject":"非線形性","subitem_subject_scheme":"Other"},{"subitem_subject":"分岐","subitem_subject_scheme":"Other"},{"subitem_subject":"two dimensional flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flutter","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flutter analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"isentropic flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"high aspect ratio wing","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aeroelasticity","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aircraft design","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aircraft structure","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wing oscillation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"limit cycle oscillation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"nonlinearity","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"bifurcation","subitem_subject_language":"en","subitem_subject_scheme":"Other"}]},"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":"conference paper","resourceuri":"http://purl.org/coar/resource_type/c_5794"}]},"item_title":"Flutter LCO in isentropic flow: Analytical theory","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Flutter LCO in isentropic flow: Analytical theory","subitem_title_language":"en"}]},"item_type_id":"5","owner":"1","path":["991","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"5662","relation_version_is_last":true,"title":["Flutter LCO in isentropic flow: Analytical theory"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T08:09:49.849540+00:00"}