{"created":"2023-06-20T14:37:01.667820+00:00","id":3395,"links":{},"metadata":{"_buckets":{"deposit":"8b156285-7ff5-4b35-84d8-0d695cc20749"},"_deposit":{"created_by":1,"id":"3395","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"3395"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00003395","sets":["1887:1891","9:789:817:824"]},"author_link":["13406","13407"],"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2017-03-15","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"42","bibliographicPageStart":"33","bibliographicVolumeNumber":"JAXA-SP-16-008E","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 the First International Symposium on Flutter and its Application","bibliographic_titleLang":"en"}]}]},"item_5_description_15":{"attribute_name":"会議概要（会議名, 開催地, 会期, 主催者等）（英）","attribute_value_mlt":[{"subitem_description":"First International Symposium on Flutter and its Application (May 15-17, 2016. Mielparque-tokyo), Minato-ku, Tokyo, Japan","subitem_description_type":"Other"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Flapping wing has been utilized in many engineering fields such as power generation, micro aerial vehicles, under water vehicles, etc.. As is well known, flapping wing motion is governed by many parameters such as frequency, heaving amplitude, pitching (or feathering) amplitude, phase difference between heaving and pitching motions for rigid wing and additional parameters such as bending and torsion rigidity, mass distribution, etc. for elastic wings. Therefore, the application of optimum design technique plays crucial role for the design of high performance devices/vehicles using flapping wing. In this paper, some applications of an optimization technique to the flapping wing designs that the present author has studied during last fifteen years of his career are outlined. They are a flutter power generation system, a micro aerial vehicle and its use for the estimation of the propulsive performance of dolphin.","subitem_description_type":"Other"}]},"item_5_description_18":{"attribute_name":"内容記述","attribute_value_mlt":[{"subitem_description":"形態: カラー図版あり","subitem_description_type":"Other"}]},"item_5_description_19":{"attribute_name":"内容記述（英）","attribute_value_mlt":[{"subitem_description":"Physical characteristics: Original contains color illustrations","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA1630046002","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-16-008E","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(JAXA)"}]},"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":"九州大学"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Kyushu University"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"磯貝, 紘二"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Isogai, Koji","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":"2020-01-15"}],"displaytype":"detail","filename":"AA1630046002.pdf","filesize":[{"value":"1.0 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"AA1630046002.pdf","url":"https://jaxa.repo.nii.ac.jp/record/3395/files/AA1630046002.pdf"},"version_id":"e9716e33-8a4c-44a4-b472-17780c9848fb"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"power generation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flapping wing MAV","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"propulsive efficiency of dolphin","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"optimum design","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":"Some applications of an optimum design technique to flapping wing designs","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Some applications of an optimum design technique to flapping wing designs","subitem_title_language":"en"}]},"item_type_id":"5","owner":"1","path":["824","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2017-04-27"},"publish_date":"2017-04-27","publish_status":"0","recid":"3395","relation_version_is_last":true,"title":["Some applications of an optimum design technique to flapping wing designs"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T09:03:34.951063+00:00"}