{"created":"2023-06-20T14:36:36.397515+00:00","id":2943,"links":{},"metadata":{"_buckets":{"deposit":"4e1fc119-f778-4ccd-9eb3-46c2cd332d9b"},"_deposit":{"created_by":1,"id":"2943","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"2943"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00002943","sets":["1398:1530:1531","1543:1874:1875","1887:1891","9:789:794:1976"]},"author_link":["10031","10033","10036","10035","10034","10032"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Performance Analyses of Fluidic Thrust Vector Control System Using DSMC Method"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2019-02-25","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"140","bibliographicPageStart":"135","bibliographicVolumeNumber":"JAXA-SP-18-005","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構特別資料: 第50回流体力学講演会/第36回航空宇宙数値シミュレーション技術シンポジウム論文集"},{"bibliographic_title":"JAXA Special Publication: Proceedings of the 50th Fluid Dynamics Conference / the 36th Aerospace Numerical Simulation Symposium","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50回流体力学講演会/第36回航空宇宙数値シミュレーション技術シンポジウム (2018年7月4日-6日. 宮崎市民プラザ), 宮崎市, 宮崎","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":"50th Fluid Dynamics Conference /the 36th Aerospace Numerical Simulation Symposium (July 4-6, 2018. Miyazaki Citizen's Plaza), Miyazaki, Japan","subitem_description_type":"Other"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Flows in the rocket engine nozzles are numerically analyzed to assess the performance of Thrust Vector Control (TVC) system of fluidic type by the Direct Simulation Monte Carlo (DSMC) method. Secondary jet is injected into the flow field through a small tube attached to either side of two-dimensional dual throat nozzle wall. The main flow separation caused by the secondary jet is observed, and the direction of the thrust vector deviates from the symmetry axis of the nozzle. However, the deviation also occurs randomly when the secondary jet is stopped, which is not intended in the TVC system. In order to avoid it and perform the infallible deviation when intended, some research for the appropriate nozzle shape and the position of the secondary jet injection is done.","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: AA1830029014","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-18-005","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_22":{"attribute_name":"ISSNONLINE","attribute_value_mlt":[{"subitem_source_identifier":"2433-2232","subitem_source_identifier_type":"ISSN"}]},"item_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"岡山理科大学"},{"subitem_text_value":"岡山理科大学"},{"subitem_text_value":"岡山理科大学"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Okayama University of Science"},{"subitem_text_language":"en","subitem_text_value":"Okayama University of Science"},{"subitem_text_language":"en","subitem_text_value":"Okayama University of Science"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"丸山, 祐一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"坂田, 政士"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"髙橋, 遥一朗"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Maruyama, Yuichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Sakata, Masashi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Takahashi, Yoichiro","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":"2020-01-15"}],"displaytype":"detail","filename":"AA1830029014.pdf","filesize":[{"value":"2.2 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"AA1830029014.pdf","url":"https://jaxa.repo.nii.ac.jp/record/2943/files/AA1830029014.pdf"},"version_id":"4a71f398-56cc-4aae-8137-ddd7f7aa3e5f"}]},"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":"DSMC 法による流体式推力方向制御装置の性能解析","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"DSMC 法による流体式推力方向制御装置の性能解析"}]},"item_type_id":"5","owner":"1","path":["1531","1875","1891","1976"],"pubdate":{"attribute_name":"公開日","attribute_value":"2019-02-28"},"publish_date":"2019-02-28","publish_status":"0","recid":"2943","relation_version_is_last":true,"title":["DSMC 法による流体式推力方向制御装置の性能解析"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T09:13:25.525546+00:00"}