{"created":"2023-06-20T15:11:02.604607+00:00","id":40627,"links":{},"metadata":{"_buckets":{"deposit":"960e8d0d-aaeb-4af9-8d60-61417878dec0"},"_deposit":{"created_by":1,"id":"40627","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"40627"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00040627","sets":["1887:1893","1896:1898:1913:1917"]},"author_link":["448964","448965"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Design and development of an oscillating system for 2-D wing models"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2000-01","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"12","bibliographicPageStart":"1","bibliographicVolumeNumber":"1403","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所報告"},{"bibliographic_title":"Technical Report of National Aerospace Laboratory","bibliographic_titleLang":"en"}]}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"低速風洞で振動翼まわりの非定常流れ現象を調べるために斬新なデザインを行った2次元翼模型加振装置を開発した。本装置の特徴は、3台のモータをパソコンで制御することにより最大8Hzの擬似正弦波加振ができるとともに、翼模型の平均仰角、振動振幅、振動数を自動的に変更可能にしている点にある。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"To investigate the unsteady flow characteristics of the oscillating two-dimensional wing, an innovative mechanism to drive two-dimensional wing models was developed. The major design concepts of the system are: (1) quasi-harmonic pitching oscillation up to frequency of 8 Hz via three electric motors controlled by the personal computer; and (2) the mean-angles of attack, the amplitude and the frequencies can be changed automatically. The system is used for the flow visualization in a low wind tunnel to view the unsteady flow patterns around an oscillating two-dimensional wing model.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0001991000","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 TR-1403","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":"0389-4010","subitem_source_identifier_type":"ISSN"}]},"item_3_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"航空宇宙技術研究所 構造研究部"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Structures Division"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"菊池, 孝男"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kikuchi, Takao","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":"2020-01-27"}],"displaytype":"detail","filename":"naltr0001403.pdf","filesize":[{"value":"1.4 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltr0001403.pdf","url":"https://jaxa.repo.nii.ac.jp/record/40627/files/naltr0001403.pdf"},"version_id":"97ed5433-e207-40fc-b376-708201c139c9"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"2次元翼","subitem_subject_scheme":"Other"},{"subitem_subject":"翼加振装置","subitem_subject_scheme":"Other"},{"subitem_subject":"振動翼","subitem_subject_scheme":"Other"},{"subitem_subject":"非定常流れ特性","subitem_subject_scheme":"Other"},{"subitem_subject":"流れの可視化","subitem_subject_scheme":"Other"},{"subitem_subject":"パーソナルコンピュータ制御","subitem_subject_scheme":"Other"},{"subitem_subject":"非定常空力特性","subitem_subject_scheme":"Other"},{"subitem_subject":"電動機駆動系","subitem_subject_scheme":"Other"},{"subitem_subject":"低速風洞","subitem_subject_scheme":"Other"},{"subitem_subject":"two dimensional wing","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wing oscillating system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"oscillating wing","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"unsteady flow characteristic","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flow visualization","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"personal computer control","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"unsteady aerodynamic characteristic","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"motor drive system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"low wind tunnel","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":"technical report","resourceuri":"http://purl.org/coar/resource_type/c_18gh"}]},"item_title":"2次元翼模型加振装置の開発","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"2次元翼模型加振装置の開発"}]},"item_type_id":"3","owner":"1","path":["1893","1917"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"40627","relation_version_is_last":true,"title":["2次元翼模型加振装置の開発"],"weko_creator_id":"1","weko_shared_id":1},"updated":"2023-06-20T19:14:14.925630+00:00"}