{"created":"2023-06-20T14:39:20.727460+00:00","id":6093,"links":{},"metadata":{"_buckets":{"deposit":"a88d4d54-6370-48ac-9d81-5a6929f4ac5b"},"_deposit":{"created_by":1,"id":"6093","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"6093"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00006093","sets":["1887:1893","9:789:1031:1037"]},"author_link":["30399","30398","30397","30401","30400","30402"],"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2006-03-31","bibliographicIssueDateType":"Issued"},"bibliographicVolumeNumber":"JAXA-SP-05-035E","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構特別資料"},{"bibliographic_title":"JAXA Special Publication","bibliographic_titleLang":"en"}]}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"This booklet provides practical information on the computational fluid dynamics of the multiphase flows in solid rocket motors with descriptions of mathematical modeling, simulation methods, computer codes, and many numerical experiments. Combustion flows of metallized composite propellants in solid rocket motors are multiphase flows consisting of particles and gas. In this booklet, descriptions are given concerning the mathematical modeling of the gas-particle interaction and its sensitivity on various parameters, simulation methods of gas-particle multiphase flows, such as, the Eulerian-Eulerian, the Eulerian-Lagrangian, and the Eulerian-hybrid methods, and the modeling method of combustion and breakup of particles, and so on. Computer programs, SPECS (Solid Propulsion Enhanced Code Series), coded along with these techniques are also introduced to the readers. Moreover, many examples of numerical experiments are provided on the verification of the mathematical modeling and numerical methods.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0063153000","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: JAXA-SP-05-035E","subitem_description_type":"Other"}]},"item_3_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙航空研究開発機構"}]},"item_3_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Japan Aerospace Exploration Agency (JAXA)"}]},"item_3_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"1349-113X","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":"AA11984031","subitem_source_identifier_type":"NCID"}]},"item_3_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"宇宙航空研究開発機構"},{"subitem_text_value":"宇宙航空研究開発機構"},{"subitem_text_value":"アイ・エイチ・アイ・エアロスペース"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency"},{"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":[{}]},{"creatorNames":[{"creatorName":"大門, 優"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"関野, 展弘"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Shimada, Toru","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Daimon, Yu","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Sekino, Nobuhiro","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":"2020-01-16"}],"displaytype":"detail","filename":"63153000.pdf","filesize":[{"value":"22.2 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"63153000.pdf","url":"https://jaxa.repo.nii.ac.jp/record/6093/files/63153000.pdf"},"version_id":"9a6bd7ab-e264-4738-8584-633f1a3bca3d"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"計算流体力学","subitem_subject_scheme":"Other"},{"subitem_subject":"固体推進剤ロケットエンジン","subitem_subject_scheme":"Other"},{"subitem_subject":"数値解析","subitem_subject_scheme":"Other"},{"subitem_subject":"数学モデル","subitem_subject_scheme":"Other"},{"subitem_subject":"オイラー・オイラー法","subitem_subject_scheme":"Other"},{"subitem_subject":"オイラー・ラグランジ法","subitem_subject_scheme":"Other"},{"subitem_subject":"オイラー・ハイブリッド法","subitem_subject_scheme":"Other"},{"subitem_subject":"固体燃料ロケットモータ","subitem_subject_scheme":"Other"},{"subitem_subject":"SRM","subitem_subject_scheme":"Other"},{"subitem_subject":"多相流","subitem_subject_scheme":"Other"},{"subitem_subject":"ガス-固体相互作用","subitem_subject_scheme":"Other"},{"subitem_subject":"化学平衡","subitem_subject_scheme":"Other"},{"subitem_subject":"燃焼","subitem_subject_scheme":"Other"},{"subitem_subject":"熱伝達","subitem_subject_scheme":"Other"},{"subitem_subject":"computational fluid dynamics","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"solid propellant rocket engine","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"numerical analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"mathematical model","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Eulerian-Eulerian method","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Eulerian-Lagrangian method","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Eulerian-hybrid method","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"solid rocket motor","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"SRM","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"multiphase flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"gas-solid interaction","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"chemical equilibrium","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"combustion","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"heat transfer","subitem_subject_language":"en","subitem_subject_scheme":"Other"}]},"item_language":{"attribute_name":"言語","attribute_value_mlt":[{"subitem_language":"eng"}]},"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":"Computational fluid dynamics of multiphase flows in solid rocket motors","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Computational fluid dynamics of multiphase flows in solid rocket motors","subitem_title_language":"en"}]},"item_type_id":"3","owner":"1","path":["1037","1893"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"6093","relation_version_is_last":true,"title":["Computational fluid dynamics of multiphase flows in solid rocket motors"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T08:02:20.670744+00:00"}