{"created":"2023-06-20T15:14:59.989062+00:00","id":45029,"links":{},"metadata":{"_buckets":{"deposit":"c9263128-0091-473d-b232-b46accef3a26"},"_deposit":{"created_by":1,"id":"45029","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"45029"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00045029","sets":["1887:1893","1896:1898:1913:1917"]},"author_link":["472575","472570","472576","472577","472572","472571","472574","472573"],"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1983-07","bibliographicIssueDateType":"Issued"},"bibliographicPageStart":"22","bibliographicVolumeNumber":"771","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所報告"},{"bibliographic_title":"Technical Report of National Aerospace Laboratory TR-771","bibliographic_titleLang":"en"}]}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"This report describes numerical schemes used in the computer program for nozzle performance predications of liquid rocket engines. The program is a set consisting of the following four programs: a program of one-dimensional equilibrium flow(ODE), a one-dimensional kinetic flow(ODK), a two-dimensional kinetic flow(TDK), and a turbulent boundary layer(TBL). Published programs were utilized for ODE and TBL, but the programs for ODK and TDK were newly developed. In the TDK program, an efficient numerical scheme for a two-dimensional nonequilibrium flow was devised for rocket nozzle flowfields, and is described in detail in this report. Computational results are presented for hydrogen/oxygen and NTO/A-50 propellant engines, showing the utility of the present computer program by comparing it with available 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: NALTR0771000","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-771","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"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Kakuda Branch Office, National Aerospace Laboratory(NAL)"},{"subitem_text_language":"en","subitem_text_value":"Kakuda Branch Office, National Aerospace Laboratory(NAL)"},{"subitem_text_language":"en","subitem_text_value":"Kakuda Branch Office, National Aerospace Laboratory(NAL)"},{"subitem_text_language":"en","subitem_text_value":"Kakuda Branch Office, National Aerospace Laboratory(NAL)"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"中橋, 和博"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"宮島, 博"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"木皿, 且人"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"毛呂, 明夫"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"NAKAHASHI, Kazuhiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"MIYAJIMA, Hiroshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"KISARA, Katsuto","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"MORO, Akio","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":"2020-01-29"}],"displaytype":"detail","filename":"naltr00771.pdf","filesize":[{"value":"1.5 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltr00771.pdf","url":"https://jaxa.repo.nii.ac.jp/record/45029/files/naltr00771.pdf"},"version_id":"d02569b9-d19e-4617-9533-5d576a591cbd"}]},"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":"ロケットノズルの性能予測計算法","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"ロケットノズルの性能予測計算法"}]},"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":"45029","relation_version_is_last":true,"title":["ロケットノズルの性能予測計算法"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:46:33.420052+00:00"}