{"created":"2023-06-20T14:53:32.556803+00:00","id":21730,"links":{},"metadata":{"_buckets":{"deposit":"8b27ad53-7e44-4a43-ac6c-f64e1a2c6342"},"_deposit":{"created_by":1,"id":"21730","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"21730"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00021730","sets":["1887:1888"]},"author_link":["203999","204004","204001","204006","204003","204005","204000","204007","204002","203998"],"item_7_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Investigation of Dynamic Characteristics of a Reentry Lifting Capsule by Free Rotation Tests in Transonic Speed"}]},"item_7_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2016-10-05","bibliographicIssueDateType":"Issued"},"bibliographicIssueNumber":"5","bibliographicPageEnd":"287(35)","bibliographicPageStart":"281(29)","bibliographicVolumeNumber":"64","bibliographic_titles":[{"bibliographic_title":"日本航空宇宙学会論文集"},{"bibliographic_title":"Journal of the Japan Society for Aeronautical and Space Sciences","bibliographic_titleLang":"en"}]}]},"item_7_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"For a design of a reentry capsule and its flight, one of the most important problems is an assessment of the dynamic stability in transonic speed. In this study, dynamic stability tests for a lifting capsule were conducted with the 1-DOF free-rotation test method in the JAXA 2m × 2m Transonic Wind Tunnel. In this test method, the reduced frequency and time history of the angular motion in non-dimensional time could be matched between the wind-tunnel test and the actual flight. Effects of flow conditions, location of center of gravity, an ablated shape, surface roughness and model MOI were discussed with the obtained time-series angular data and schlieren photographs. Furthermore, a new data processing method was developed for calculating the damping coefficients. The obtained amplitude and frequency of the oscillations, and the estimated damping coefficients give helpful information for the project planning.","subitem_description_type":"Other"}]},"item_7_description_18":{"attribute_name":"内容記述","attribute_value_mlt":[{"subitem_description":"形態: 図版あり","subitem_description_type":"Other"}]},"item_7_description_19":{"attribute_name":"内容記述（英）","attribute_value_mlt":[{"subitem_description":"Physical characteristics: Original contains illustrations","subitem_description_type":"Other"}]},"item_7_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: DS1640221005","subitem_description_type":"Other"}]},"item_7_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"Japan Society for Aeronautical and Space Sciences"}]},"item_7_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"日本航空宇宙学会"}]},"item_7_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"1344-6460","subitem_source_identifier_type":"ISSN"}]},"item_7_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AA11307372","subitem_source_identifier_type":"NCID"}]},"item_access_right":{"attribute_name":"アクセス権","attribute_value_mlt":[{"subitem_access_right":"metadata only access","subitem_access_right_uri":"http://purl.org/coar/access_right/c_14cb"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"古賀, 星吾"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"互井, 梨絵"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"日高, 亜希子"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"中野, 英一郎"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"永井, 伸治"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Koga, Seigo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Tagai, Rie","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hidaka, Akiko","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nakano, Eiichiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nagai, Shinji","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"Reentry Capsule","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Transonic Dynamic Stability","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Wind Tunnel Testing","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":"journal article","resourceuri":"http://purl.org/coar/resource_type/c_6501"}]},"item_title":"自由回転試験による揚力カプセルの遷音速動特性の考察","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"自由回転試験による揚力カプセルの遷音速動特性の考察"}]},"item_type_id":"7","owner":"1","path":["1888"],"pubdate":{"attribute_name":"公開日","attribute_value":"2016-11-01"},"publish_date":"2016-11-01","publish_status":"0","recid":"21730","relation_version_is_last":true,"title":["自由回転試験による揚力カプセルの遷音速動特性の考察"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T03:31:23.679294+00:00"}