{"created":"2023-06-20T14:39:47.849750+00:00","id":6595,"links":{},"metadata":{"_buckets":{"deposit":"67ee5e7a-5059-4756-856c-b8ed2a4eb178"},"_deposit":{"created_by":1,"id":"6595","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"6595"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00006595","sets":["1887:1891","9:789:1085:1365"]},"author_link":["33748","33752","33750","33751","33754","33753","33749","33755"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Wind tunnel test using scaled model rotor system"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2004-03-25","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"50","bibliographicPageStart":"44","bibliographicVolumeNumber":"JAXA-SP-03-003","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構特別資料: 第66回　風洞研究会議論文集"},{"bibliographic_title":"JAXA Special Publication: Proceedings of the Wind Tunnel Technology Association 66th Meeting","bibliographic_titleLang":"en"}]}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"This paper presents the outline of the scaled model rotor system, which was used in 2 m by 2 m FHI low-speed wind tunnel, and some typical wind tunnel tests. The scaled model rotor system has been applied for many fundamental tests and development tests since 1991. The system consists of teetering type hub, blades, pylon, rotary balance and servomotor etc. The collective pitch and cyclic pitch can be changed with remote control.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0047428006","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-03-003","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"}]},"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":"富士重工業"},{"subitem_text_value":"富士重工業"},{"subitem_text_value":"富士重工業"},{"subitem_text_value":"富士重工業"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Fuji Heavy Industries Ltd."},{"subitem_text_language":"en","subitem_text_value":"Fuji Heavy Industries Ltd."},{"subitem_text_language":"en","subitem_text_value":"Fuji Heavy Industries Ltd."},{"subitem_text_language":"en","subitem_text_value":"Fuji Heavy Industries Ltd."}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"塚原, 孝則"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"橋口, 祐子"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"太田, 智基"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"小生方, 正裕"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Tsukahara, Takanori","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hashiguchi, Yuko","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ota, Tomoki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Obukata, Masahiro","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":"47428006.pdf","filesize":[{"value":"1.7 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"47428006.pdf","url":"https://jaxa.repo.nii.ac.jp/record/6595/files/47428006.pdf"},"version_id":"e431911d-2050-46c7-b657-ff3197002138"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"ヘリコプタ","subitem_subject_scheme":"Other"},{"subitem_subject":"風洞試験","subitem_subject_scheme":"Other"},{"subitem_subject":"風洞模型","subitem_subject_scheme":"Other"},{"subitem_subject":"ロータダイナミクス","subitem_subject_scheme":"Other"},{"subitem_subject":"ロータブレード","subitem_subject_scheme":"Other"},{"subitem_subject":"騒音低減","subitem_subject_scheme":"Other"},{"subitem_subject":"振動減衰","subitem_subject_scheme":"Other"},{"subitem_subject":"低層音翼端","subitem_subject_scheme":"Other"},{"subitem_subject":"helicopter","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wind tunnel test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wind tunnel model","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"rotor dynamics","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"rotor blade","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"noise reduction","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"vibration damping","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"low noise wing tip","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":"conference 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