{"created":"2023-06-20T15:08:32.376597+00:00","id":38015,"links":{},"metadata":{"_buckets":{"deposit":"48e57bb9-9645-4167-9376-cdf99262bda6"},"_deposit":{"created_by":1,"id":"38015","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"38015"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00038015","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["431172","431171"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Flutter of non-planar wing model including lateral mode effects"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2001-02","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"83","bibliographicPageStart":"79","bibliographicVolumeNumber":"51","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所特別資料: 第64回・第65回風洞研究会議論文集"},{"bibliographic_title":"Special Publication of National Aerospace Laboratory: Proceedings of the 64th and 65th Workshop on Wind Tunnel Research","bibliographic_titleLang":"en"}]}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"In a case that a reentry winged space vehicle with non-planar wings like tip-fin is attached atop of a launch rocket, lateral modes due to attachments between the vehicle and the rocket or/and elasticity of the rocket may effect to flutter characteristics of the wings. A particular supporting system was developed, which had a yawing elasticity as a lateral mode. Flutter experiments were made in NAL-TWT. Also, flutter characteristics were computed by using DPM (Doublet-Point Method). Numerical results are consistent with experimental results.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0032235010","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: NAL SP-51","subitem_description_type":"Other"}]},"item_5_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"航空宇宙技術研究所"}]},"item_5_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"National Aerospace Laboratory (NAL)"}]},"item_5_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0289-260X","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":"AN10097345","subitem_source_identifier_type":"NCID"}]},"item_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"航空宇宙技術研究所"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"神田, 淳"}],"nameIdentifiers":[{"nameIdentifier":"431171","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Kanda, Atsushi","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"431172","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":"2020-01-24"}],"displaytype":"detail","filename":"nalsp0051010.pdf","filesize":[{"value":"513.3 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0051010.pdf","url":"https://jaxa.repo.nii.ac.jp/record/38015/files/nalsp0051010.pdf"},"version_id":"875d224f-060b-4738-ba94-ee5757510c47"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"翼","subitem_subject_scheme":"Other"},{"subitem_subject":"宇宙機","subitem_subject_scheme":"Other"},{"subitem_subject":"フラッタ解析","subitem_subject_scheme":"Other"},{"subitem_subject":"宇宙機モデル","subitem_subject_scheme":"Other"},{"subitem_subject":"横振動","subitem_subject_scheme":"Other"},{"subitem_subject":"有限要素モデル","subitem_subject_scheme":"Other"},{"subitem_subject":"力学的性質","subitem_subject_scheme":"Other"},{"subitem_subject":"剛体","subitem_subject_scheme":"Other"},{"subitem_subject":"wing","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerospace vehicle","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flutter analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aircraft model","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"lateral oscillation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"finite element method","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"mechanical property","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"rigid structure","subitem_subject_language":"en","subitem_subject_scheme":"Other"}]},"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":"conference paper","resourceuri":"http://purl.org/coar/resource_type/c_5794"}]},"item_title":"非平面翼の横モードが連成するフラッタ","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"非平面翼の横モードが連成するフラッタ"}]},"item_type_id":"5","owner":"1","path":["1891","1915"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"38015","relation_version_is_last":true,"title":["非平面翼の横モードが連成するフラッタ"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T22:46:36.924962+00:00"}