{"created":"2023-06-20T15:02:46.017198+00:00","id":31848,"links":{},"metadata":{"_buckets":{"deposit":"2cb9b1b2-3721-4d4b-a486-fa4650645abe"},"_deposit":{"created_by":1,"id":"31848","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"31848"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00031848","sets":["1887:1890","1896:1898:1899:1910"]},"author_link":["406495","406497","406498","406499","406496","406494"],"item_9_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Characteristics of the Blow-down Type Hypersonic Wind Tunnel of Institute of Space and Aeronautical Science, University of Tokyo"}]},"item_9_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1966-07","bibliographicIssueDateType":"Issued"},"bibliographicIssueNumber":"3_A","bibliographicPageEnd":"873","bibliographicPageStart":"839","bibliographicVolumeNumber":"2","bibliographic_titles":[{"bibliographic_title":"東京大学宇宙航空研究所報告"}]}]},"item_9_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"東大宇宙研に新設された直径200mmのfree jet吹出式極超音速風洞の測定部における圧力分布,温度分布および空気力などの測定を行なった実験結果を報告する.使用したノズルは設計マッハ数7,8および9の三種である.よどみ点圧力および温度は,気流軸を中心にして直径120mmの円形断面内で一箱流が実現されており力の測定も良い結果を得た.したがってこの風洞の設計目標は一応達成されていると考えられる","subitem_description_type":"Abstract"}]},"item_9_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Present paper gives measured results of pressure and temperature distributions in the test chamber of a blow-down tope hypersonic wind tunnel constructed at Institute of Space and Aeronautical Science, University of Tokyo. Designed Mach numbers of the nozzles used in the experiment are 7,8 and 9, and exit diameter of each nozzle is zoomm. The results show that the stagnation prssure and temperature are almost uniform within circular cross section of 120mm diameter, the axis of which is aligned with the flow axis.","subitem_description_type":"Other"}]},"item_9_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: SA0124905000","subitem_description_type":"Other"}]},"item_9_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"東京大学宇宙航空研究所"}]},"item_9_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0563-8100","subitem_source_identifier_type":"ISSN"}]},"item_9_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AN00161914","subitem_source_identifier_type":"NCID"}]},"item_9_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"東京大学宇宙航空研究所航空力学部"},{"subitem_text_value":"東京大学宇宙航空研究所航空力学部"},{"subitem_text_value":"東京大学宇宙航空研究所航空力学部"}]},"item_9_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"the Institute of Space and Aeronautical Science University of Tokyo"},{"subitem_text_language":"en","subitem_text_value":"the Institute of Space and Aeronautical Science University of Tokyo"},{"subitem_text_language":"en","subitem_text_value":"the Institute of Space and Aeronautical Science University of Tokyo"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"河村, 龍馬"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"辛島, 桂一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"関, 和市"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"KAWAMURA, Ryuma","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"KARASHIMA, Keiichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"SEKI, Kazuichi","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":"2020-01-24"}],"displaytype":"detail","filename":"SA0124905.pdf","filesize":[{"value":"1.5 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"SA0124905.pdf","url":"https://jaxa.repo.nii.ac.jp/record/31848/files/SA0124905.pdf"},"version_id":"6f65b224-76a8-4b7e-8b09-bada2fae2457"}]},"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":"departmental bulletin paper","resourceuri":"http://purl.org/coar/resource_type/c_6501"}]},"item_title":"東大宇宙航空研究所極超音速風洞の特性","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"東大宇宙航空研究所極超音速風洞の特性"}]},"item_type_id":"9","owner":"1","path":["1890","1910"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"31848","relation_version_is_last":true,"title":["東大宇宙航空研究所極超音速風洞の特性"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T00:48:45.851015+00:00"}