{"created":"2023-06-20T14:37:49.561270+00:00","id":4271,"links":{},"metadata":{"_buckets":{"deposit":"49d1f7e9-13d8-46ed-945d-a05a1504cf3e"},"_deposit":{"created_by":1,"id":"4271","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"4271"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00004271","sets":["1398:1530:1537","1543:1874:1881","1887:1891","9:789:888:896"]},"author_link":["18747","18744","18741","18746","18745","18740","18743","18742"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"CFD Analysis of Rocket Plumes during Landing of a Reusable Sounding Rocket"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2013-03-29","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"190","bibliographicPageStart":"185","bibliographicVolumeNumber":"JAXA-SP-12-010","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構特別資料"},{"bibliographic_title":"JAXA Special Publication: Proceedings of 44th Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2012","bibliographic_titleLang":"en"}]}]},"item_5_description_14":{"attribute_name":"会議概要（会議名, 開催地, 会期, 主催者等）","attribute_value_mlt":[{"subitem_description":"第44回流体力学講演会/航空宇宙数値シミュレーション技術シンポジウム2012 (2012年7月5日-6日. 富山国際会議場大手町フォーラム), 富山市, 富山県","subitem_description_type":"Other"}]},"item_5_description_15":{"attribute_name":"会議概要（会議名, 開催地, 会期, 主催者等）（英）","attribute_value_mlt":[{"subitem_description":"44th Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2012 (July 5-6, 2012. Toyama International Conference Center), Toyama Japan","subitem_description_type":"Other"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Through a numerical simulation, we investigated the effects of rocket plumes on heating in vertical landing of a reusable sounding rocket. A simulation was carried out by using an in-house compressible flow solver, LS FLOW-RG, which is applicable to real gas phenomena, multi-species gas, chemical reactions and so on. This is an extended version of LS-FLOW of JAXA/JEDI center. In this solver, the transport properties of muti-species gas and mass conservation equations of those species are considered. On the other hand, we employed DDES method as a turbulence model. In this simulation, flow conditions of rocket plumes are of high temperature (T=2000K) and supersonic (M=3.0) water vapor, and an atmospheric condition is a stationary standard air. In this study, we assumed the actual landing condition and body. In fact, jets blow off from two engines at the bottom of the body. In this situation, we compared the results in two different thrust condi\"\"\" tions of rocket plumes and discussed the heating effect by thrust levels in vertical landing. From the results, we confirmed that a pair of jets generates circulation between the earth and the bottom of the body, and this phenomenon promotes the diffusion of high temperature water vapor. Furthermore, the difference of thrust level largely affected both flow and thermal fields on the bottom of the body.","subitem_description_type":"Other"}]},"item_5_description_18":{"attribute_name":"内容記述","attribute_value_mlt":[{"subitem_description":"形態: カラー図版あり","subitem_description_type":"Other"}]},"item_5_description_19":{"attribute_name":"内容記述（英）","attribute_value_mlt":[{"subitem_description":"Physical characteristics: Original contains color illustrations","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0061958031","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: JAXA-SP-12-010","subitem_description_type":"Other"}]},"item_5_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙航空研究開発機構(JAXA)"}]},"item_5_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Japan Aerospace Exploration Agency (JAXA)"}]},"item_5_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"1349-113X","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":"AA11984031","subitem_source_identifier_type":"NCID"}]},"item_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"宇宙航空研究開発機構情報・計算工学センター(JAXA)(JEDIC)"},{"subitem_text_value":"宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS)"},{"subitem_text_value":"株式会社計算力学研究センター"},{"subitem_text_value":"宇宙航空研究開発機構情報・計算工学センター(JAXA)(JEDIC)"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"JAXA'ｓ Engineering Digital Innovation Center, Japan Aerospace Exploration Agency (JAXA)(JEDIC)"},{"subitem_text_language":"en","subitem_text_value":"Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)（ISAS）"},{"subitem_text_language":"en","subitem_text_value":"Research Center of Computational Mechanics, Inc."},{"subitem_text_language":"en","subitem_text_value":"JAXA'ｓ Engineering Digital Innovation Center, Japan Aerospace Exploration Agency (JAXA)(JEDIC)"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"葛生, 和人"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"野中, 聡"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"青野, 淳也"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"嶋, 英志"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kuzuu, Kazuto","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nonaka, Satoshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Aono, Junya","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Shima, Eiji","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":"61958031.pdf","filesize":[{"value":"1.2 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"61958031.pdf","url":"https://jaxa.repo.nii.ac.jp/record/4271/files/61958031.pdf"},"version_id":"09272ab5-ea7b-4e61-86ef-cf3ac1fbb0d0"}]},"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":"再使用観測ロケット着陸時プルームのCFD解析","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"再使用観測ロケット着陸時プルームのCFD解析"}]},"item_type_id":"5","owner":"1","path":["896","1537","1881","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"4271","relation_version_is_last":true,"title":["再使用観測ロケット着陸時プルームのCFD解析"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T08:43:33.559918+00:00"}