{"created":"2023-06-20T14:36:14.141149+00:00","id":2547,"links":{},"metadata":{"_buckets":{"deposit":"bcb341b1-1a36-448b-b06f-3bce046d5b18"},"_deposit":{"created_by":1,"id":"2547","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"2547"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00002547","sets":["1887:1893","9:1090:1186:1202"]},"author_link":["7163","7164","7168","7165","7166","7167"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Aerodynamic Characteristics of Blimp Models by Wind tunnel Tests"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2012-02-10","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"34","bibliographicPageStart":"1","bibliographicVolumeNumber":"JAXA-RM-11-008","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構研究開発資料"},{"bibliographic_title":"JAXA Research and Development Memorandum","bibliographic_titleLang":"en"}]}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"小型飛行船の設計や飛行シミュレーションおよび飛行制御則を構築する上で，小型飛行船の空力特性を把握することが求められている．そのため，風洞試験用模型として船体長1 m の船体模型，種々の尾翼模型，およびゴンドラ模型を製作し，それらを組み合わせた模型により風洞試験を実施して空力特性を取得した．  ","subitem_description_type":"Abstract"},{"subitem_description":"  本報告は，風洞試験で得られた小型飛行船模型の空力特性データを，グラフに整理して提示するものである．","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The aerodynamic characteristics of blimps need to be grasped because of the design of blimps, flight simulations, and flight control design. The hull model of hull length 1 m, various tail models, and gondola models were manufactured as the models for wind tunnel tests. The wind tunnel tests by the models were carried out.  ","subitem_description_type":"Other"},{"subitem_description":"  This report shows in the graphs the aerodynamic characteristics data of the blimp models obtained by the wind tunnel tests.","subitem_description_type":"Other"}]},"item_3_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_3_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_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0065138000","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: JAXA-RM-11-008","subitem_description_type":"Other"}]},"item_3_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙航空研究開発機構(JAXA)"}]},"item_3_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Japan Aerospace Exploration Agency (JAXA)"}]},"item_3_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"1349-1121","subitem_source_identifier_type":"ISSN"}]},"item_3_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AA11983593","subitem_source_identifier_type":"NCID"}]},"item_3_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"宇宙航空研究開発機構航空プログラムグループ無人機・未来型航空機チーム (JAXA)"},{"subitem_text_value":"神戸大学大学院工学研究科"},{"subitem_text_value":"宇宙航空研究開発機構研究開発本部風洞技術開発センター (JAXA)"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Unmanned and Innovative aircraft Team, Aviation Program Group, Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Graduate School of Engineering, Kobe University"},{"subitem_text_language":"en","subitem_text_value":"Wind Tunnel Technology Center, Aerospace Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA)"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"奥山, 政広"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"深尾, 隆則"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"岩崎, 昭人"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Okuyama, Masahiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Fukao, Takanori","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Iwasaki, Akihito","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":"65138000.pdf","filesize":[{"value":"2.0 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"65138000.pdf","url":"https://jaxa.repo.nii.ac.jp/record/2547/files/65138000.pdf"},"version_id":"f9083e3f-ca55-4590-b3a4-eedeb0ad61b7"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"Blimp","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Model","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Tail","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Wind Tunnel Test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Aerodynamic Characteristics","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":"風洞試験による小型飛行船模型の空力特性","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"風洞試験による小型飛行船模型の空力特性"}]},"item_type_id":"3","owner":"1","path":["1202","1893"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"2547","relation_version_is_last":true,"title":["風洞試験による小型飛行船模型の空力特性"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T09:20:21.875182+00:00"}