{"created":"2023-06-20T14:37:43.592503+00:00","id":4143,"links":{},"metadata":{"_buckets":{"deposit":"cae4ce5c-c300-413c-b173-463dec45b24c"},"_deposit":{"created_by":1,"id":"4143","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"4143"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00004143","sets":["1887:1891","9:789:868:887"]},"author_link":["17890","17886","17888","17889","17887","17894","17893","17895","17892","17891"],"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2013-11-30","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"405","bibliographicPageStart":"397","bibliographicVolumeNumber":"JAXA-SP-13-001E","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構特別資料"},{"bibliographic_title":"JAXA Special Publication","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":"5th Symposium on Integrating CFD and Experiments in Aerodynamics (October 3-5, 2012, Chofu Aerospace Center, Japan Aerospace Exploration Agency (JAXA)), Chofu, Tokyo, Japan","subitem_description_type":"Other"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The purpose of this study is to measure the unsteady force acting on a slender delta wing in two degree-of-freedom (DoF) motion. A serial-type robot manipulator was used to oscillate the model in two modes; one is roll-yaw coupled lateral motion and the other is pitch-heave coupled longitudinal motion. Unsteady forces and moments were measured by a six-component balance and the effects of oscillation frequency and amplitude were evaluated. In the 2-DoF roll-yaw coupled mode, hysteresis loop was noted at high angles of attack and changes of rolling moment are delayed as compared with the 1-DoF case. In the pitch-heave coupled experiment, it was found that the effect of pitch rate on unsteady force is negligible at the frequency and amplitude ranges covered in this experiment.","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: AA0062070035","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-13-001E","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":"東北大学大学院工学研究科"},{"subitem_text_value":"東北大学大学院工学研究科"},{"subitem_text_value":"東北大学大学院工学研究科"},{"subitem_text_value":"東北大学大学院工学研究科"},{"subitem_text_value":"東北大学大学院工学研究科"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Graduate School of Engineering, Tohoku University"},{"subitem_text_language":"en","subitem_text_value":"Graduate School of Engineering, Tohoku University"},{"subitem_text_language":"en","subitem_text_value":"Graduate School of Engineering, Tohoku University"},{"subitem_text_language":"en","subitem_text_value":"Graduate School of Engineering, Tohoku University"},{"subitem_text_language":"en","subitem_text_value":"Graduate School of Engineering, Tohoku University"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"原, 達矢"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"沼田, 大樹"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"浅井, 圭介"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"伊藤, 崇文"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"姜, 欣"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hara, Tatsuya","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Numata, Daiju","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Asai, Keisuke","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ito, Takafumi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Jiang, Xin","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":"62070035.pdf","filesize":[{"value":"569.6 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"62070035.pdf","url":"https://jaxa.repo.nii.ac.jp/record/4143/files/62070035.pdf"},"version_id":"5ea6154a-0c85-4583-97f8-4a80630d8604"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"Dynamic Wind-Tunnel Testing","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Multi-Degree-of-Freedom","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Robotic Manipulator","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Delta Wing","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Vortex Breakdown","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":"Dynamic Wind-Tunnel Testing of a Delta Wing Using a Multi-Degree-of-Freedom Robotic Manipulator","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Dynamic Wind-Tunnel Testing of a Delta Wing Using a Multi-Degree-of-Freedom Robotic Manipulator","subitem_title_language":"en"}]},"item_type_id":"5","owner":"1","path":["887","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"4143","relation_version_is_last":true,"title":["Dynamic Wind-Tunnel Testing of a Delta Wing Using a Multi-Degree-of-Freedom Robotic Manipulator"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T08:46:21.728034+00:00"}