{"created":"2023-06-20T14:39:08.184607+00:00","id":5814,"links":{},"metadata":{"_buckets":{"deposit":"70b959b9-3cd0-428b-b0b8-f246ac4a66c0"},"_deposit":{"created_by":1,"id":"5814","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"5814"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00005814","sets":["1887:1891","9:789:998:1008"]},"author_link":["28575","28574","28571","28578","28573","28572","28576","28577"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Flow-deflection angle calibration of JAXA 0.44 m Hypersonic Shock Tunnel"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2007-03-28","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"32","bibliographicPageStart":"15","bibliographicVolumeNumber":"JAXA-SP-06-026","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構特別資料: 第77回風洞研究会議論文集"},{"bibliographic_title":"JAXA Special Publication: Proceedings of the Wind Tunnel Technology Association 77th Meeting","bibliographic_titleLang":"en"}]}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Flow-deflection angle calibration tests were conducted at JAXA 0.44 m Hypersonic Shock Tunnel with a dual-wheel model support system. Surface pressures on upper and lower surfaces of a two-dimensional wedge model were measured to identify the flow deflection angle. The flow around the model was visualized by a schlieren optical system. The tests were conducted at a nominal Mach number of 10.4. The flow-deflection angle was deducted as 0.2 degrees.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0063333003","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-06-026","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":"宇宙航空研究開発機構"},{"subitem_text_value":"宇宙航空研究開発機構"},{"subitem_text_value":"宇宙航空研究開発機構"},{"subitem_text_value":"宇宙航空研究開発機構"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"山崎, 喬"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"中北, 和之"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"中川, 宗敬"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"渡利, 實"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yamazaki, Takashi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nakakita, Kazuyuki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nakagawa, Muneyoshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Watari, Minoru","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":"63333003.pdf","filesize":[{"value":"2.4 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"63333003.pdf","url":"https://jaxa.repo.nii.ac.jp/record/5814/files/63333003.pdf"},"version_id":"315f75c0-6e31-4e0e-bf19-3decd14969f9"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"気流偏向","subitem_subject_scheme":"Other"},{"subitem_subject":"極超音速衝撃風洞","subitem_subject_scheme":"Other"},{"subitem_subject":"極超音速流","subitem_subject_scheme":"Other"},{"subitem_subject":"感圧塗料","subitem_subject_scheme":"Other"},{"subitem_subject":"圧力測定","subitem_subject_scheme":"Other"},{"subitem_subject":"測定装置","subitem_subject_scheme":"Other"},{"subitem_subject":"風洞模型","subitem_subject_scheme":"Other"},{"subitem_subject":"シュリーレン写真法","subitem_subject_scheme":"Other"},{"subitem_subject":"流れの可視化","subitem_subject_scheme":"Other"},{"subitem_subject":"flow deflection","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"hypersonic shock tunnel","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"hypersonic flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"pressure sensitive paint","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"pressure measurement","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"measuring instrument","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wind tunnel model","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Schlieren photography","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flow visualization","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":"JAXA0.44m極超音速衝撃風洞と気流偏向特性試験","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"JAXA0.44m極超音速衝撃風洞と気流偏向特性試験"}]},"item_type_id":"5","owner":"1","path":["1008","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"5814","relation_version_is_last":true,"title":["JAXA0.44m極超音速衝撃風洞と気流偏向特性試験"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T08:08:11.556119+00:00"}