{"created":"2023-06-20T14:47:03.300474+00:00","id":14676,"links":{},"metadata":{"_buckets":{"deposit":"3cdb072c-03f2-44c8-ad75-03513e529f9e"},"_deposit":{"created_by":1,"id":"14676","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"14676"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00014676","sets":["1543:1656:1669","1887:1891"]},"author_link":["134076","134078","134081","134079","134080","134082","134083","134077"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Study on flowfield around winged TSTO launch vehicle by visualization using the electrical discharge method"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2004-05","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"122","bibliographicPageStart":"119","bibliographic_titles":[{"bibliographic_title":"宇宙航行の力学シンポジウム　平成15年度"},{"bibliographic_title":"Symposium on Flight Mechanics and Astrodynamics 2003","bibliographic_titleLang":"en"}]}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The visualization of flowfield around a winged TSTO (Two Stage To Orbit) launch vehicle model has been carried out using the electrical discharge method. In this report, boundary layers and three-dimensional (lateral and cross-sectional) shock shapes around the model are demonstrated. The existence of a separation shock is confirmed three-dimensionally. The experiments are carried out using a hypersonic gun tunnel, with Mach number of 10 and duration of 10 ms.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0047120031","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本部"}]},"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":"福山大学 大学院"},{"subitem_text_value":"福山大学 大学院"},{"subitem_text_value":"福山大学 工学部"},{"subitem_text_value":"宇宙航空研究開発機構 総合技術研究本部"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Fukuyama University Graduate School"},{"subitem_text_language":"en","subitem_text_value":"Fukuyama University Graduate School"},{"subitem_text_language":"en","subitem_text_value":"Fukuyama University Faculty of Engineering"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics"}]},"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":"瀬崎, 新士"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"中村, 弘明"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"西尾, 正富"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"山本, 行光"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Sezaki, Shinji","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nakamura, Hiroaki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nishio, Masatomi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yamamoto, Yukimitsu","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"再使用型宇宙機","subitem_subject_scheme":"Other"},{"subitem_subject":"TSTO","subitem_subject_scheme":"Other"},{"subitem_subject":"再使用型打上げ機","subitem_subject_scheme":"Other"},{"subitem_subject":"衝撃波-境界層干渉","subitem_subject_scheme":"Other"},{"subitem_subject":"極超音速飛行","subitem_subject_scheme":"Other"},{"subitem_subject":"流れの可視化","subitem_subject_scheme":"Other"},{"subitem_subject":"風洞試験","subitem_subject_scheme":"Other"},{"subitem_subject":"境界層剥離","subitem_subject_scheme":"Other"},{"subitem_subject":"放電","subitem_subject_scheme":"Other"},{"subitem_subject":"reusable spacecraft","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"TSTO","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"reusable launch vehicle","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"shock wave-boundary layer interaction","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"hypersonic flight","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flow visualization","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wind tunnel test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"boundary layer separation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"electric discharge","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":"有翼TSTO宇宙往還機周りの流れ場の放電発光法による可視化研究","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"有翼TSTO宇宙往還機周りの流れ場の放電発光法による可視化研究"}]},"item_type_id":"5","owner":"1","path":["1669","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"14676","relation_version_is_last":true,"title":["有翼TSTO宇宙往還機周りの流れ場の放電発光法による可視化研究"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T05:31:04.620798+00:00"}