{"created":"2023-06-20T14:39:08.140591+00:00","id":5813,"links":{},"metadata":{"_buckets":{"deposit":"5881138f-41f2-4301-8b49-5669ff871658"},"_deposit":{"created_by":1,"id":"5813","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"5813"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00005813","sets":["1887:1891","9:789:998:1008"]},"author_link":["28555","28553","28562","28565","28563","28569","28552","28551","28554","28558","28561","28567","28560","28556","28557","28566","28568","28564","28559","28570"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Calibration of the test section Mach number in the JAXA 2 m x 2 m Transonic Wind Tunnel"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2007-03-28","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"14","bibliographicPageStart":"6","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":"In the JAXA 2 m x 2 m Transonic Wind Tunnel, there have been more needs of wind tunnel users for high measurement accuracy to develop aircraft and launch vehicles with high performance. To achieve higher accuracy, more elaborate calibration tests to calculate freestream flow conditions have been conducted in this wind tunnel. To obtain test section Mach numbers exactly, test section static pressures must be measured precisely. However, the measurement of test section static pressure is difficult for transonic flows, especially high subsonic flows because of probe nose effects, blockage effects, support interference, and so on. A series of calibration tests is conducted to optimize the static pressure probe for transonic flows and to determine the test section Mach number in the model location from the plenum chamber Mach number.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0063333002","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"},{"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":"コスモテック"},{"subitem_text_value":"コスモテック"},{"subitem_text_value":"IHIエアロスペース・エンジニアリング"}]},"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"},{"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":"Cosmotec Co. Ltd."},{"subitem_text_language":"en","subitem_text_value":"Cosmotec Co. Ltd."},{"subitem_text_language":"en","subitem_text_value":"IHI Aerospace Engineering Co. Ltd."}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"香西, 政孝"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"上野, 真"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"塩原, 辰郎"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"小松, 行夫"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"唐澤, 敏夫"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"小池, 陽"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"須谷, 記和"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"我那覇, 義人"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"今, 直樹"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"原口, 智裕"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kozai, Masataka","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ueno, Makoto","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Shiohara, Tatsuro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Komatsu, Yukio","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Karasawa, Toshio","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Koike, Akira","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Sudani, Norikazu","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ganaha, Yoshito","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kon, Naoki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Haraguchi, Tomohiro","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":"63333002.pdf","filesize":[{"value":"1.4 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"63333002.pdf","url":"https://jaxa.repo.nii.ac.jp/record/5813/files/63333002.pdf"},"version_id":"af251fbb-141a-4b71-ac98-418effe07002"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"遷音速風洞","subitem_subject_scheme":"Other"},{"subitem_subject":"風洞試験","subitem_subject_scheme":"Other"},{"subitem_subject":"マッハ数","subitem_subject_scheme":"Other"},{"subitem_subject":"検定","subitem_subject_scheme":"Other"},{"subitem_subject":"静圧","subitem_subject_scheme":"Other"},{"subitem_subject":"測定装置","subitem_subject_scheme":"Other"},{"subitem_subject":"精度","subitem_subject_scheme":"Other"},{"subitem_subject":"遷音速流","subitem_subject_scheme":"Other"},{"subitem_subject":"圧力測定","subitem_subject_scheme":"Other"},{"subitem_subject":"transonic wind tunnel","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wind tunnel test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Mach number","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"calibration","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"static pressure","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"measuring instrument","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"accuracy","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"transonic flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"pressure measurement","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":"JAXA2m×2m遷音速風洞における測定部マッハ数検定試験","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"JAXA2m×2m遷音速風洞における測定部マッハ数検定試験"}]},"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":"5813","relation_version_is_last":true,"title":["JAXA2m×2m遷音速風洞における測定部マッハ数検定試験"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T08:08:12.804769+00:00"}