{"created":"2023-06-20T15:08:45.779146+00:00","id":38249,"links":{},"metadata":{"_buckets":{"deposit":"4316c852-a8bc-434b-96a0-7e6ab5ad2f32"},"_deposit":{"created_by":1,"id":"38249","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"38249"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00038249","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["432463","432464","432466","432465"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Numerical simulation of internal multi-phase flow in solid rocket motor"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2003-03","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"159","bibliographicPageStart":"154","bibliographicVolumeNumber":"57","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所特別資料: 航空宇宙数値シミュレーション技術シンポジウム2002論文集"},{"bibliographic_title":"Special Publication of National Aerospace Laboratory: Proceedings of Aerospace Numerical Simulation Symposium 2002","bibliographic_titleLang":"en"}]}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Comparison is made between two methods, Eulerian and Lagrangian, of describing the particle-phase behavior in multi-phase flow in solid rocket motors. A newly developed CFD code, SPEC2, is used to evaluate the latter approach. The results show significant difference especially where particle streams are crossing and at the limiting particle streamlines. Merits and demerits of both methods are also discussed.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0045948028","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-57","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":"宇宙科学研究所"},{"subitem_text_value":"アイ・エイチ・アイ・エアロスペース"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Institute of Space and Astronautical Science"},{"subitem_text_language":"en","subitem_text_value":"IHI Aerospace Co. Ltd."}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"嶋田, 徹"}],"nameIdentifiers":[{"nameIdentifier":"432463","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"関野, 展弘"}],"nameIdentifiers":[{"nameIdentifier":"432464","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Shimada, Toru","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"432465","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Sekino, Nobuhiro","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"432466","nameIdentifierScheme":"WEKO"}]}]},"item_files":{"attribute_name":"ファイル情報","attribute_type":"file","attribute_value_mlt":[{"accessrole":"open_date","date":[{"dateType":"Available","dateValue":"2020-01-24"}],"displaytype":"detail","filename":"nalsp0057028.pdf","filesize":[{"value":"583.6 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0057028.pdf","url":"https://jaxa.repo.nii.ac.jp/record/38249/files/nalsp0057028.pdf"},"version_id":"f94dc03e-fe34-4321-9e0e-c0dd4e70599d"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"CFD","subitem_subject_scheme":"Other"},{"subitem_subject":"多相流","subitem_subject_scheme":"Other"},{"subitem_subject":"数値シミュレーション","subitem_subject_scheme":"Other"},{"subitem_subject":"固体モーターロケット","subitem_subject_scheme":"Other"},{"subitem_subject":"Euler法","subitem_subject_scheme":"Other"},{"subitem_subject":"Lagrange法","subitem_subject_scheme":"Other"},{"subitem_subject":"Navier-Stokes方程式","subitem_subject_scheme":"Other"},{"subitem_subject":"計算グリッド","subitem_subject_scheme":"Other"},{"subitem_subject":"エネルギー保存","subitem_subject_scheme":"Other"},{"subitem_subject":"研究開発","subitem_subject_scheme":"Other"},{"subitem_subject":"圧力分布","subitem_subject_scheme":"Other"},{"subitem_subject":"温度分布","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"multiphase flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"numerical simulation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"solid rocket motor","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Euler method","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Lagrange method","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Navier-Stokes equation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"computational grid","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"energy conservation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"research and development","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"pressure distribution","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"temperature distribution","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":"固体ロケット内部混相流解析:粒子相記述法による相違","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"固体ロケット内部混相流解析:粒子相記述法による相違"}]},"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":"38249","relation_version_is_last":true,"title":["固体ロケット内部混相流解析:粒子相記述法による相違"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T22:42:58.240617+00:00"}