{"created":"2023-06-20T14:37:49.517738+00:00","id":4270,"links":{},"metadata":{"_buckets":{"deposit":"66bd7c61-bcee-491b-b688-e4a11ecc787d"},"_deposit":{"created_by":1,"id":"4270","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"4270"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00004270","sets":["1398:1530:1537","1543:1874:1881","1887:1891","9:789:888:896"]},"author_link":["18734","18736","18735","18737","18733","18732","18738","18739"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Aerodynamic Characteristics and Kinematic Analysis during Turnover 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":"184","bibliographicPageStart":"179","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":"Flight performance of a reusable sounding rocket during turnover was investigated by numerical analysis. In this　study, we first carried out the numerical flow simulation to obtain aerodynamic characteristics in dynamic conditions. This simulation is based on three dimensional unsteady full Navier-Stokes equation, and a flow field is solved by an in-house code, LS-FLOW. After that, we solved kinematic equations of a rotational rigid body using obtained dynamic characteristics. This analysis is also carried out numerically by using the 4th order Runge-Kutta method. The calculated body is of a simple baseline shape whose aerodynamic parts, fins, strakes, canards and so on are not attached. However, simulated conditions are based on the actual flight environment. For validation, we first compared the numerical flow simulation with the wind tunnel test data in a static condition where an attack angle of the body is fixed. Agreement of those resu\"\"\" lts is satisfactory. From the results under the dynamic conditions, we could evaluate the dynamic damping characteristics of pitching moment during turnover maneuver. As a result, we confirmed that the breakdown of the longitudinal vortices during turnover largely affects flight performance rather than the dynamic damping effect.","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: AA0061958030","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":"61958030.pdf","filesize":[{"value":"1.2 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"61958030.pdf","url":"https://jaxa.repo.nii.ac.jp/record/4270/files/61958030.pdf"},"version_id":"e72d4a1e-aa7b-47a1-801c-83a6dc970f75"}]},"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転回飛行における空力特性と運動解析","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"再使用観測ロケット転回飛行における空力特性と運動解析"}]},"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":"4270","relation_version_is_last":true,"title":["再使用観測ロケット転回飛行における空力特性と運動解析"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T08:43:34.479272+00:00"}