{"created":"2023-06-20T14:48:23.740174+00:00","id":16195,"links":{},"metadata":{"_buckets":{"deposit":"52546277-2a93-4d4e-8d36-62d144f0f8b8"},"_deposit":{"created_by":1,"id":"16195","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"16195"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00016195","sets":["1543:1693:1700","1887:1891"]},"author_link":["146980","146981","146973","146975","146982","146979","146974","146972","146976","146977","146971","146978"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Airframe Drag Assessment Based on Wind Tunnel Tests of a Small-scale Supersonic Flight Experiment Vehicle"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2013-01","bibliographicIssueDateType":"Issued"},"bibliographic_titles":[{"bibliographic_title":"平成24年度宇宙輸送シンポジウム: 講演集録"},{"bibliographic_title":"Proceedings of Space Transportation Symposium: FY2012","bibliographic_titleLang":"en"}]}]},"item_5_description_14":{"attribute_name":"会議概要（会議名, 開催地, 会期, 主催者等）","attribute_value_mlt":[{"subitem_description":"平成24年度宇宙輸送シンポジウム (2013年1月17日-1月18日. 宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS)), 相模原市, 神奈川県","subitem_description_type":"Other"}]},"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":"Space Transportation FY2012 (January 17-18, 2013. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)), Sagamihara, Kanagawa Japan","subitem_description_type":"Other"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"With the aims of creating and validating innovative fundamental technologies for high-speed atmospheric flights, a small-scale supersonic experimental vehicle is being developed as a flying test bed. The configuration M2006 with a cranked-arrow main wing and twin engines was designed and its aerodynamic characteristics were verified through wind-tunnel and flight tests. A new configuration M2011 with a main wing and tails of similar shapes and a single GG-ATR engine was proposed. Intensive wind-tunnel tests were carried out in transonic and supersonic regimes. It was found that the overall drag coefficient increases as the intake passage is throttled and that the airflow through the intake seems to be squeezed by the development of the boundary layer. In addition, the tail steering box located at the vertical tail root has little influence on overall drag.","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"},{"subitem_description":"形態: PDF","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"},{"subitem_description":"Physical characteristics: PDF","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0061856059","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: STCP-2012-059","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宇宙科学研究所(JAXA)(ISAS)"}]},"item_5_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)"}]},"item_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"室蘭工業大学航空宇宙機システム研究センター"},{"subitem_text_value":"室蘭工業大学航空宇宙機システム研究センター"},{"subitem_text_value":"室蘭工業大学航空宇宙機システム研究センター"},{"subitem_text_value":"室蘭工業大学航空宇宙機システム研究センター"},{"subitem_text_value":"室蘭工業大学航空宇宙機システム研究センター"},{"subitem_text_value":"室蘭工業大学航空宇宙機システム研究センター"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Aerospace Plane Research Center, Muroran Institute of Technology"},{"subitem_text_language":"en","subitem_text_value":"Aerospace Plane Research Center, Muroran Institute of Technology"},{"subitem_text_language":"en","subitem_text_value":"Aerospace Plane Research Center, Muroran Institute of Technology"},{"subitem_text_language":"en","subitem_text_value":"Aerospace Plane Research Center, Muroran Institute of Technology"},{"subitem_text_language":"en","subitem_text_value":"Aerospace Plane Research Center, Muroran Institute of Technology"},{"subitem_text_language":"en","subitem_text_value":"Aerospace Plane Research Center, Muroran Institute of Technology"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"大石, 栄"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"溝端, 一秀"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"湊, 亮二郎"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"高木, 正平"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"東野, 和幸"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"棚次, 亘弘"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Oishi, Sakae","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Mizobata, Kazuhide","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Minato, Ryojiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Takagi, Shohei","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Higashino, Kazuyuki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Tanatsugu, Nobuhiro","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":"2020-01-20"}],"displaytype":"detail","filename":"61856059.pdf","filesize":[{"value":"2.9 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"61856059.pdf","url":"https://jaxa.repo.nii.ac.jp/record/16195/files/61856059.pdf"},"version_id":"fac1b726-6d86-471e-9bc6-995e3f77aaf2"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"Drag","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Supersonic","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Aerodynamic Characterization","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Flying Test Bed","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 paper","resourceuri":"http://purl.org/coar/resource_type/c_5794"}]},"item_title":"小型超音速飛行実験機の風洞試験に基づく機体抗力検討","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"小型超音速飛行実験機の風洞試験に基づく機体抗力検討"}]},"item_type_id":"5","owner":"1","path":["1700","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"16195","relation_version_is_last":true,"title":["小型超音速飛行実験機の風洞試験に基づく機体抗力検討"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T04:58:11.782315+00:00"}