{"created":"2023-06-20T14:37:48.689481+00:00","id":4251,"links":{},"metadata":{"_buckets":{"deposit":"62962382-1a81-4f44-a35d-6a474aa5264b"},"_deposit":{"created_by":1,"id":"4251","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"4251"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00004251","sets":["1398:1530:1537","1543:1874:1881","1887:1891","9:789:888:896"]},"author_link":["18570","18572","18571","18573"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Development of Overset CFD Technology in Unstructured, Compressible Flow Solver for Arbitrary Polyhedral Meshes, LS-FLOW"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2013-03-29","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"66","bibliographicPageStart":"61","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":"The overset grid approach provides a very powerful means of handling complex geometries in computational fluid dynamics. The overset grid approach has many practical benefits for unsteady moving grid simulation or rudder angle. Therefore an overset unstructured grid method was newly developed for an arbitrary polyhedral compressible flow solver, LS-FLOW. We set the IBlank for visualization and post-processing. In order to test the validity of the suggested methods, a numerical simulation was carried out on the NACA0012 airfoil.And our results are compared with experimental data and other CFD results. Furthermore, in order to evaluate the validity of this method, we also simulated the flow around a reusable sounding rocket under research at JAXA//ISAS. The result of the overset grid method corresponds with the result of the single grid method in the NACA0012 airfoil and the reusable sounding rocket. The good coincidence validates our newly deve\"\"\" loped overset grid method, and intend to use LS-FLOW as a design tool.","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: AA0061958011","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":"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":"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":"青野, 淳也"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"葛生, 和人"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Aono, Junya","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kuzuu, Kazuto","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":"61958011.pdf","filesize":[{"value":"1.4 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"61958011.pdf","url":"https://jaxa.repo.nii.ac.jp/record/4251/files/61958011.pdf"},"version_id":"a878a50b-7bc4-4ed7-9d71-7207cbd1dc85"}]},"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":"任意多面体非構造圧縮性ソルバーLS-FLOWにおける重合格子法開発","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"任意多面体非構造圧縮性ソルバーLS-FLOWにおける重合格子法開発"}]},"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":"4251","relation_version_is_last":true,"title":["任意多面体非構造圧縮性ソルバーLS-FLOWにおける重合格子法開発"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T08:43:56.013471+00:00"}