{"created":"2023-06-20T15:13:24.642359+00:00","id":43343,"links":{},"metadata":{"_buckets":{"deposit":"55f85ef1-9b02-4ea6-89ed-95c355162757"},"_deposit":{"created_by":1,"id":"43343","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"43343"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00043343","sets":["1887:1893","1896:1898:1913:1915"]},"author_link":["463305","463306","463308","463307"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Numerical Simulation on Inverse Jet of Solid Rocket Motor"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1989-11","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"86","bibliographicPageStart":"81","bibliographicVolumeNumber":"10","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 SP-10","bibliographic_titleLang":"en"}]}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Solid particle laden two-phase inverse jet flows are studied numerically. A TVD-Upwind scheme for the gas-phase and a Flux-Vector-Splitting-Upwind scheme for the particle-phase are used to solve the two-phase Euler equations. The Eulerian formulation for the two-phase Euler flow problem is simpler in theoretical structure and more economical in computational time than the Lagrangian formulation. Numerical simulations on the single-phase and two-phase inverse jets shows the influence of solid particles on a nozzle and the flow field. An instability of the two-phase flow is also observed probably because of a numerical error.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALSP0010014","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 SP-10","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":"0289-260X","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":"AN10097345","subitem_source_identifier_type":"NCID"}]},"item_3_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"名古屋大学工学部航空学科"},{"subitem_text_value":"三菱重工業株式会社"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Department of Aeronautical Engineering, Nagoya University"},{"subitem_text_language":"en","subitem_text_value":"Mitsubishi Heavy Industries Co.Ltd."}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"林, 光一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"松田, 実"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hayashi, Koichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Matsuda, Minoru","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":"2020-01-28"}],"displaytype":"detail","filename":"nalsp0010014.pdf","filesize":[{"value":"549.0 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0010014.pdf","url":"https://jaxa.repo.nii.ac.jp/record/43343/files/nalsp0010014.pdf"},"version_id":"ff2c716a-60f0-41ab-82c4-e676b19bec10"}]},"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":"固体ロケットにおける逆噴射ジェットの数値シミュレーション","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"固体ロケットにおける逆噴射ジェットの数値シミュレーション"}]},"item_type_id":"3","owner":"1","path":["1893","1915"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"43343","relation_version_is_last":true,"title":["固体ロケットにおける逆噴射ジェットの数値シミュレーション"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T22:16:56.113674+00:00"}