{"created":"2023-06-20T15:07:24.509859+00:00","id":36780,"links":{},"metadata":{"_buckets":{"deposit":"b28b5ecf-6d8f-48b5-97db-440bcedfed4f"},"_deposit":{"created_by":1,"id":"36780","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"36780"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00036780","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["477563","477562","477569","477564","477565","477570","477571","477566","477559","477567","477568","477572","477573","477574","477561","477560"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Analysis of mixing flows for the hypersupersonic transport propulsion system"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1996-01","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"68","bibliographicPageStart":"65","bibliographicVolumeNumber":"30","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所特別資料"},{"bibliographic_title":"Special Publication of National Aerospace Laboratory","bibliographic_titleLang":"en"}]}]},"item_5_description_14":{"attribute_name":"会議概要（会議名, 開催地, 会期, 主催者等）","attribute_value_mlt":[{"subitem_description":"航空宇宙技術研究所 7-9 Jun. 1995 東京 日本","subitem_description_type":"Other"}]},"item_5_description_15":{"attribute_name":"会議概要（会議名, 開催地, 会期, 主催者等）（英）","attribute_value_mlt":[{"subitem_description":"National Aerospace Laboratory 7-9 Jun. 1995 Tokyo Japan","subitem_description_type":"Other"}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"超音速機用推進システムにはさまざな混合を伴う流れがある。例えば、離陸時の騒音レベルを下げるためのミキサエジェクタノズル内における排気ジェットと取入空気との混合、燃焼モード切り換え時における前部混合部でのラム側空気とターボ側空気の混合などである。本推進システムの研究開発においては、このような混合流の特性を予測することがシステム設計や性能改善にとって重要である。ここでは、前述のミキサエジェクタノズルおよび前部混合部の混合流について、数値計算と試験データの比較例を報告する。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"There are lots of the mixing flows on the hypersupersonic transport propulsion system. For instance, the mixing between the exhaust jet and the entrained flow in the mixer-ejector nozzle to reduce the noise level at the take off and the mixing between the ram air and the turbo air in the front mixing component operating for the dual mode of the the hypersupersonic transport propulsion system. In the research and the development of this system it is very useful for predicting the mixing characteristics to design components and improve the performance of this system. In this paper the comparison between the analysis results and the test results of above two kinds flows are reported.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0000294012","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: NAL SP-30","subitem_description_type":"Other"}]},"item_5_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"航空宇宙技術研究所"}]},"item_5_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"National Aerospace Laboratory (NAL)"}]},"item_5_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0289-260X","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":"AN10097345","subitem_source_identifier_type":"NCID"}]},"item_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"石川島播磨重工業"},{"subitem_text_value":"石川島播磨重工業"},{"subitem_text_value":"石川島播磨重工業"},{"subitem_text_value":"石川島播磨重工業"},{"subitem_text_value":"東京理科大学"},{"subitem_text_value":"航空宇宙技術研究所"},{"subitem_text_value":"航空宇宙技術研究所"},{"subitem_text_value":"航空宇宙技術研究所"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Ishikawajima-Harima Heavy Industries Co Ltd"},{"subitem_text_language":"en","subitem_text_value":"Ishikawajima-Harima Heavy Industries Co Ltd"},{"subitem_text_language":"en","subitem_text_value":"Ishikawajima-Harima Heavy Industries Co Ltd"},{"subitem_text_language":"en","subitem_text_value":"Ishikawajima-Harima Heavy Industries Co Ltd"},{"subitem_text_language":"en","subitem_text_value":"Science University of Tokyo"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"大石, 勉"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"平井, 健二"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"児玉, 秀和"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"宮城, 裕幸"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"山本, 誠"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"田村, 敦宏"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"菊地, 一雄"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"野崎, 理"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Oishi, Tsutomu","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hirai, Kenji","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kodama, Hidekazu","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Miyagi, Hiroyuki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yamamoto, Makoto","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Tamura, Atsuhiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kikuchi, Kazuo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nozaki, Osamu","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":"2020-02-10"}],"displaytype":"detail","filename":"nalsp0030012.pdf","filesize":[{"value":"285.2 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0030012.pdf","url":"https://jaxa.repo.nii.ac.jp/record/36780/files/nalsp0030012.pdf"},"version_id":"0a5bfdbc-abec-4dd2-80ae-ea3dbbf03daf"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"ラムジェット機関","subitem_subject_scheme":"Other"},{"subitem_subject":"超音速機","subitem_subject_scheme":"Other"},{"subitem_subject":"混合流れ","subitem_subject_scheme":"Other"},{"subitem_subject":"ミキサエジェクタノズル","subitem_subject_scheme":"Other"},{"subitem_subject":"騒音抑制","subitem_subject_scheme":"Other"},{"subitem_subject":"排気ジェット","subitem_subject_scheme":"Other"},{"subitem_subject":"空気取入口","subitem_subject_scheme":"Other"},{"subitem_subject":"モード切換","subitem_subject_scheme":"Other"},{"subitem_subject":"乱流混合","subitem_subject_scheme":"Other"},{"subitem_subject":"流れ特性","subitem_subject_scheme":"Other"},{"subitem_subject":"乱流モデル","subitem_subject_scheme":"Other"},{"subitem_subject":"格子形成","subitem_subject_scheme":"Other"},{"subitem_subject":"模型試験","subitem_subject_scheme":"Other"},{"subitem_subject":"推進システム","subitem_subject_scheme":"Other"},{"subitem_subject":"ramjet engine","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"hypersupersonic transport","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"supersonic mixing flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"mixer ejector nozzle","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"noise control","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"exhaust jet","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"air intake inlet","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"mode changing","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"turbulent mixing","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flow characteristic","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"turbulent flow model","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"grid generation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"model test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"propulsion system","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":"超音速機用推進システムにおける混合流解析","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"超音速機用推進システムにおける混合流解析"}]},"item_type_id":"5","owner":"1","path":["1891","1915"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"36780","relation_version_is_last":true,"title":["超音速機用推進システムにおける混合流解析"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:31:46.819994+00:00"}