{"created":"2023-06-20T15:11:30.011955+00:00","id":41172,"links":{},"metadata":{"_buckets":{"deposit":"cd713389-6375-4363-acbb-6cb38eba2a75"},"_deposit":{"created_by":1,"id":"41172","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"41172"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00041172","sets":["1887:1893","1896:1898:1913:1917"]},"author_link":["450924","450927","450922","450920","450928","450921","450923","450931","450925","450929","450926","450930"],"item_3_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"スクラムジェット前縁モデルにおける熱伝達の研究"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1992-12","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"16","bibliographicPageStart":"1","bibliographicVolumeNumber":"1187T","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所報告"},{"bibliographic_title":"Technical Report of National Aerospace Laboratory","bibliographic_titleLang":"en"}]}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"スクラムジェットエンジンのインレットやストラット前縁部を模擬した冷却構造パネルの加熱試験および解析を行なった。円弧型の前縁部を持つニッケル電鋳製の冷却パネルを超音速の高温ガス流中で加熱した。ガス発生器として、NTO(4酸化2窒素)/MMH(モノメチルヒドラジン)を酸化剤および燃料とする矩形燃焼器を使用した。ガス発生器出口の一様流マッハ数は約2.67である。冷却材として水を使用し、冷却水温の上昇から熱流束分布を測定した。2次元のCFD(計算流体力学)コードおよび有限要素法コードによる解析を行ない、実験結果と比較した。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Heating tests and analysis of a cooling panel that simulates the leading edge of the scramjet engine inlet or strut were performed using crossflow type water-cooled panel with a circular leading edge. The cooling panel was fabricated by nickel electroforming and heated by supersonic hot gas. An NTO (Nitrogen TetraOxide) and MMH (MonoMethyl Hydrazine) rectangular chamber was used as the gas generator. The free stream Mach number at the nozzle exit was about 2.67. Water was used as the coolant and heat flux distribution was measured based on the temperature increase. Thermal analysis were performed using a two-dimensional CFD (Computational Fluid Dynamics) code and a finite element code. The results of the analysis were compared with the experimental data.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0004202000","subitem_description_type":"Other"}]},"item_3_description_33":{"attribute_name":"レポート番号","attribute_value_mlt":[{"subitem_description":"レポート番号: NAL TR-1187T","subitem_description_type":"Other"}]},"item_3_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"航空宇宙技術研究所"}]},"item_3_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"National Aerospace Laboratory (NAL)"}]},"item_3_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0389-4010","subitem_source_identifier_type":"ISSN"}]},"item_3_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"航空宇宙技術研究所 角田支所"},{"subitem_text_value":"航空宇宙技術研究所 角田支所"},{"subitem_text_value":"航空宇宙技術研究所 角田支所"},{"subitem_text_value":"航空宇宙技術研究所 角田支所"},{"subitem_text_value":"航空宇宙技術研究所 角田支所"},{"subitem_text_value":"石川島播磨重工業"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Kakuda Research Center"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Kakuda Research Center"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Kakuda Research Center"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Kakuda Research Center"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Kakuda Research Center"},{"subitem_text_language":"en","subitem_text_value":"Ishikawajima-Harima Heavy Industries Co Ltd"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"植田, 修一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"櫻中, 登"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"斎藤, 俊仁"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"伊藤, 勝宏"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"若松, 義男"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"今井, 究"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ueda, Shuichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Sakuranaka, Noboru","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Saito, Toshihito","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ito, Katsuhiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Wakamatsu, Yoshio","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Imai, Kiwamu","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":"2020-01-27"}],"displaytype":"detail","filename":"naltr1187t.pdf","filesize":[{"value":"999.7 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltr1187t.pdf","url":"https://jaxa.repo.nii.ac.jp/record/41172/files/naltr1187t.pdf"},"version_id":"9686b3fd-f073-4271-8dea-bfe101a1a74b"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"スクラムジェットエンジン","subitem_subject_scheme":"Other"},{"subitem_subject":"前縁加熱","subitem_subject_scheme":"Other"},{"subitem_subject":"空力加熱","subitem_subject_scheme":"Other"},{"subitem_subject":"超音速流れ","subitem_subject_scheme":"Other"},{"subitem_subject":"冷却構造","subitem_subject_scheme":"Other"},{"subitem_subject":"冷却パネル","subitem_subject_scheme":"Other"},{"subitem_subject":"性能試験","subitem_subject_scheme":"Other"},{"subitem_subject":"アクティブクーリング","subitem_subject_scheme":"Other"},{"subitem_subject":"再生冷却","subitem_subject_scheme":"Other"},{"subitem_subject":"熱防護","subitem_subject_scheme":"Other"},{"subitem_subject":"熱流束測定","subitem_subject_scheme":"Other"},{"subitem_subject":"熱伝達","subitem_subject_scheme":"Other"},{"subitem_subject":"クロスフロー型冷却パネル","subitem_subject_scheme":"Other"},{"subitem_subject":"熱構造解析","subitem_subject_scheme":"Other"},{"subitem_subject":"NTO/MMHガス発生器","subitem_subject_scheme":"Other"},{"subitem_subject":"scramjet engine","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"leading edge heating","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic heating","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"supersonic flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"cooling structure","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"cooling panel","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"performance test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"active cooling","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"regenerative cooling","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"thermal protection","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"heat flux measurement","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"heat transfer","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"crossflow type cooling panel","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"thermostructrural analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"NTO/MMH gas generator","subitem_subject_language":"en","subitem_subject_scheme":"Other"}]},"item_language":{"attribute_name":"言語","attribute_value_mlt":[{"subitem_language":"eng"}]},"item_resource_type":{"attribute_name":"資源タイプ","attribute_value_mlt":[{"resourcetype":"technical report","resourceuri":"http://purl.org/coar/resource_type/c_18gh"}]},"item_title":"A study on heat transfer in a scramjet leading edge model","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"A study on heat transfer in a scramjet leading edge model","subitem_title_language":"en"}]},"item_type_id":"3","owner":"1","path":["1893","1917"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"41172","relation_version_is_last":true,"title":["A study on heat transfer in a scramjet leading edge model"],"weko_creator_id":"1","weko_shared_id":1},"updated":"2023-06-20T19:12:43.651974+00:00"}