{"created":"2023-06-20T15:10:44.255307+00:00","id":40311,"links":{},"metadata":{"_buckets":{"deposit":"0ea6563a-4bb0-41ef-b464-6398387b6ad7"},"_deposit":{"created_by":1,"id":"40311","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"40311"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00040311","sets":["1887:1893","1896:1898:1913:1917"]},"author_link":["447268","447270","447273","447272","447266","447274","447267","447275","447269","447271"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Mach 6 testing of a scramjet engine model"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1998-07","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"20","bibliographicPageStart":"1","bibliographicVolumeNumber":"1364","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":"ラムジェット推進研究部においてラムジェットエンジン試験設備の飛行マッハ数6条件下で、スクラムジェットサブスケールエンジンの試験を行った。天板に短ストラットを取り付けることにより、良好な燃焼状態および高い燃焼効率が達成され、燃焼により発生した推力は流入気流による抗力に匹敵した。良好な燃焼が達成された後は、着火・保炎用のプラズマジェットを切った後も燃焼が持続した。燃料流量が少ない場合には別の燃焼モードが現れ、燃料は僅かに燃焼したに過ぎなかった。ステップからの燃料の平行噴射は良好な燃焼状態を阻害した。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Testing of a subscale scramjet research engine model was carried out in the Mach 6 Ramjet engine Test Facility of the National Aerospace Laboratory, Kakuda Research Center. With attachment of a short strut on the top wall, intensive combustion with high combustion efficiency was attained, and the engine produced thrust canceled the drag. The flame was held in the low velocity region around the step, even after the igniters had been turned off. When the fuel flow rate was small, there was a different combustion mode with weak combustion and little thrust. Tangential injection of fuel inhibited intensive combustion.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0001671000","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-1364","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":"1347-4588","subitem_source_identifier_type":"ISSN"}]},"item_3_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AN00311347","subitem_source_identifier_type":"NCID"}]},"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 ラムジェット推進研究部"},{"subitem_text_value":"航空宇宙技術研究所 ラムジェット推進研究部"},{"subitem_text_value":"航空宇宙技術研究所 ラムジェット推進研究部"},{"subitem_text_value":"航空宇宙技術研究所 ラムジェット推進研究部"},{"subitem_text_value":"航空宇宙技術研究所 ラムジェット推進研究部"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Ramjet Propulsion Research Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Ramjet Propulsion Research Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Ramjet Propulsion Research Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Ramjet Propulsion Research Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Ramjet Propulsion Research Division"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"苅田, 丈士"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"斎藤, 俊仁"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"工藤, 賢司"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"小室, 智幸"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"小野, 文衛"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kanda, Takeshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Saito, Toshihito","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kudo, Kenji","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Komuro, Tomoyuki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ono, Fumiei","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":"naltr0001364.pdf","filesize":[{"value":"703.7 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltr0001364.pdf","url":"https://jaxa.repo.nii.ac.jp/record/40311/files/naltr0001364.pdf"},"version_id":"d123fe08-e20a-41db-88ce-73b4642100f6"}]},"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":"エンジン燃焼試験","subitem_subject_scheme":"Other"},{"subitem_subject":"マッハ数","subitem_subject_scheme":"Other"},{"subitem_subject":"超音速燃焼","subitem_subject_scheme":"Other"},{"subitem_subject":"超音速流","subitem_subject_scheme":"Other"},{"subitem_subject":"短ストラット","subitem_subject_scheme":"Other"},{"subitem_subject":"燃料流量","subitem_subject_scheme":"Other"},{"subitem_subject":"推力","subitem_subject_scheme":"Other"},{"subitem_subject":"燃料噴射法","subitem_subject_scheme":"Other"},{"subitem_subject":"scramjet engine","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"engine combustion test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Mach number","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"supersonic combustion","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"supersonic flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"short strut","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"fuel flow rate","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"thrust","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"fuel injection method","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":"technical report","resourceuri":"http://purl.org/coar/resource_type/c_18gh"}]},"item_title":"飛行マッハ数6条件におけるスクラムジェットエンジンモデルの試験","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"飛行マッハ数6条件におけるスクラムジェットエンジンモデルの試験"}]},"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":"40311","relation_version_is_last":true,"title":["飛行マッハ数6条件におけるスクラムジェットエンジンモデルの試験"],"weko_creator_id":"1","weko_shared_id":1},"updated":"2023-06-20T19:15:43.037294+00:00"}