{"created":"2023-06-19T10:28:47.941161+00:00","id":8348,"links":{},"metadata":{"_buckets":{"deposit":"fe9c1d7d-1719-4d58-b8d6-caa3ca798f34"},"_deposit":{"created_by":18,"id":"8348","owners":[18],"pid":{"revision_id":0,"type":"depid","value":"8348"},"status":"published"},"_oai":{"id":"oai:muroran-it.repo.nii.ac.jp:00008348","sets":["35:175"]},"author_link":["38166","50634","9542","38167"],"item_77_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2001-11-30","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"84","bibliographicPageStart":"77","bibliographicVolumeNumber":"51","bibliographic_titles":[{"bibliographic_title":"室蘭工業大学紀要","bibliographic_titleLang":"ja"},{"bibliographic_title":"Memoirs of the Muroran Institute of Technology","bibliographic_titleLang":"en"}]}]},"item_77_description_23":{"attribute_name":"フォーマット","attribute_value_mlt":[{"subitem_description":"application/pdf","subitem_description_type":"Other"}]},"item_77_description_7":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"To investigate the fiow and combustian in a Scrarmjet engine model at about Mach 7 condition a small high enthalpy shock tunnel was used. A couple of wedge was set in the test section as a Scramjet engine intake and combustion chamber model. The compression process used the oblique shock systems, which was generated by vehicle edge (fore-body) and cowl, was observed. H2 and/or C2H2-air mixture gas was injected normally to supersonic cross flow in thc combustion chamber. A self-emission from combustion gas was observed by using a very high-speed video camera (18,000fps) with image intcnsifier. The wal1 static pressure in the combustion chamber was also measured. It was clarified that the wall pressure increased when the supersonic combustion occurred.","subitem_description_language":"en","subitem_description_type":"Abstract"}]},"item_77_description_8":{"attribute_name":"注記","attribute_value_mlt":[{"subitem_description":"小特集 : 「室蘭工大における航空宇宙工学研究の新展開」","subitem_description_language":"ja","subitem_description_type":"Other"}]},"item_77_publisher_11":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"室蘭工業大学","subitem_publisher_language":"ja"}]},"item_77_relation_15":{"attribute_name":"論文ID（NAID）","attribute_value_mlt":[{"subitem_relation_type":"isIdenticalTo","subitem_relation_type_id":{"subitem_relation_type_id_text":"110000076573","subitem_relation_type_select":"NAID"}}]},"item_77_source_id_12":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"13442708","subitem_source_identifier_type":"PISSN"}]},"item_77_source_id_14":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AA11175464","subitem_source_identifier_type":"NCID"}]},"item_77_subject_9":{"attribute_name":"日本十進分類法","attribute_value_mlt":[{"subitem_subject":"538","subitem_subject_scheme":"NDC"}]},"item_77_version_type_21":{"attribute_name":"著者版フラグ","attribute_value_mlt":[{"subitem_version_resource":"http://purl.org/coar/version/c_970fb48d4fbd8a85","subitem_version_type":"VoR"}]},"item_access_right":{"attribute_name":"アクセス権","attribute_value_mlt":[{"subitem_access_right":"open 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ジロウ","creatorNameLang":"ja-Kana"}],"familyNames":[{},{},{}],"givenNames":[{},{},{}],"nameIdentifiers":[{}]},{"creatorAffiliations":[{"affiliationNameIdentifiers":[],"affiliationNames":[{"affiliationName":""}]}],"creatorNames":[{"creatorName":"小久保, 崇","creatorNameLang":"ja"},{"creatorName":"KOKUBO, Takashi","creatorNameLang":"en"},{"creatorName":"コクボ, タカシ","creatorNameLang":"ja-Kana"}],"familyNames":[{},{},{}],"givenNames":[{},{},{}],"nameIdentifiers":[{}]},{"creatorAffiliations":[{"affiliationNameIdentifiers":[],"affiliationNames":[{"affiliationName":""}]}],"creatorNames":[{"creatorName":"向井, 幸司","creatorNameLang":"ja"},{"creatorName":"MUKAI, Koji","creatorNameLang":"en"},{"creatorName":"ムカイ, コウジ","creatorNameLang":"ja-Kana"}],"familyNames":[{},{},{}],"givenNames":[{},{},{}],"nameIdentifiers":[{}]}]},"item_files":{"attribute_name":"ファイル情報","attribute_type":"file","attribute_value_mlt":[{"accessrole":"open_date","date":[{"dateType":"Available","dateValue":"2016-02-16"}],"displaytype":"detail","filename":"51-77.pdf","filesize":[{"value":"3.6 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"51-77.pdf","objectType":"fulltext","url":"https://muroran-it.repo.nii.ac.jp/record/8348/files/51-77.pdf"},"version_id":"4e0ec6a2-4c43-4630-9c93-c5060fd9c250"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"scramjet engine","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"supersonic combustion","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"shock systems","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"high enthalpy shock tunnel","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":"departmental bulletin paper","resourceuri":"http://purl.org/coar/resource_type/c_6501"}]},"item_title":"小型高エンタルピー衝撃風洞を用いたスクラムジェットエンジンモデル内の超音速燃焼","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"小型高エンタルピー衝撃風洞を用いたスクラムジェットエンジンモデル内の超音速燃焼","subitem_title_language":"ja"},{"subitem_title":"Study on Flows and Combustion Phenomena in Scramjet Engine Used bu A Small Scale High Enthalpy Shock Tunnel","subitem_title_language":"en"}]},"item_type_id":"77","owner":"18","path":["175"],"pubdate":{"attribute_name":"PubDate","attribute_value":"2007-06-06"},"publish_date":"2007-06-06","publish_status":"0","recid":"8348","relation_version_is_last":true,"title":["小型高エンタルピー衝撃風洞を用いたスクラムジェットエンジンモデル内の超音速燃焼"],"weko_creator_id":"18","weko_shared_id":-1},"updated":"2024-01-24T07:13:14.859832+00:00"}