{"created":"2023-06-20T15:08:34.446037+00:00","id":38058,"links":{},"metadata":{"_buckets":{"deposit":"fa2a9ebe-73a7-4586-b619-0c7ade4191b6"},"_deposit":{"created_by":1,"id":"38058","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"38058"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00038058","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["431459","431460","431466","431464","431458","431462","431461","431465","431463","431467"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Flow analysis around ONERA Model M5 configuration using CASPER"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2002-01","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"136","bibliographicPageStart":"131","bibliographicVolumeNumber":"53","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所特別資料: 航空宇宙数値シミュレーション技術シンポジウム2001論文集"},{"bibliographic_title":"Special Publication of National Aerospace Laboratory: Proceedings of Aerospace Numerical Simulation Symposium 2001","bibliographic_titleLang":"en"}]}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The CASPER (Computational Aerodynamics System for Performance Evaluation and Research) was developed at TRDI-JDA (Technical Research and Development Institute of Japan Defense Agency) in 1998. An unstructured grid technique has a good flexibility for a complex geometry, and already its usefulness has been demonstrated for full aircraft computations. In the three-dimensional, high-Reynolds number viscous flow, the very fine and stretched grids are required to resolve accuately thin boundary layers developed along the body surface. In this paper, RANS (Reynolds-Averaged Navier-Stokes) computations are carried out in transonic and high Reynolds number flows around an ONERA Model M5 configuration by using a Spalart-Allmaras one-equation turbulence model on a hybrid unstructured grid system. With respect to pressure distributions, CL-a, CL-CD and CM-CL curves, and boundary layer transition lines, the present computed results are quantitatively compared with other computed results and wind-tunnel testing data. Especially, the drag prediction is considerately improved by the flowing strategies: (1) High resolution of surface grids around each leading edge; (2) Extension of NUM (Normalized Unstructured Mesh) method; and (3) Modification of transition parameters such as C13 and C14 in the Spalart-Allmaras one-equation model.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0032819022","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: NAL SP-53","subitem_description_type":"Other"}]},"item_5_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"航空宇宙技術研究所"}]},"item_5_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"National Aerospace Laboratory (NAL)"}]},"item_5_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0289-260X","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":"AN10097345","subitem_source_identifier_type":"NCID"}]},"item_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"防衛庁 技術研究本部"},{"subitem_text_value":"防衛庁 技術研究本部"},{"subitem_text_value":"三菱重工業"},{"subitem_text_value":"三菱重工業"},{"subitem_text_value":"菱友計算"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Japan Defense Agency Technical Research and Development Institute"},{"subitem_text_language":"en","subitem_text_value":"Japan Defense Agency Technical Research and Development Institute"},{"subitem_text_language":"en","subitem_text_value":"Mitsubishi Heavy Industries Ltd."},{"subitem_text_language":"en","subitem_text_value":"Mitsubishi Heavy Industries Ltd."},{"subitem_text_language":"en","subitem_text_value":"Ryoyu Keisan Co. Ltd."}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"沖, 良篤"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"酒田, 威志"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"内山, 直樹"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"前田, 一郎"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"安藤, 武"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Oki, Yoshiatsu","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Sakata, Takeshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Uchiyama, Naoki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Maeda, Ichiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ando, Takeshi","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":"2020-01-24"}],"displaytype":"detail","filename":"nalsp0053022.pdf","filesize":[{"value":"2.2 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0053022.pdf","url":"https://jaxa.repo.nii.ac.jp/record/38058/files/nalsp0053022.pdf"},"version_id":"8de1dc78-09dc-41be-9d84-9f565cf08514"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"空気力学","subitem_subject_scheme":"Other"},{"subitem_subject":"計算流体力学","subitem_subject_scheme":"Other"},{"subitem_subject":"非構造グリッド","subitem_subject_scheme":"Other"},{"subitem_subject":"粘性流","subitem_subject_scheme":"Other"},{"subitem_subject":"乱流モデル","subitem_subject_scheme":"Other"},{"subitem_subject":"風洞試験","subitem_subject_scheme":"Other"},{"subitem_subject":"レイノルズ平均ナビエ-ストークス方程式","subitem_subject_scheme":"Other"},{"subitem_subject":"空力特性","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamics","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"computational fluid dynamics","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"unstructured grid","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"viscous flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"turbulence model","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wind tunnel test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Reynolds averaged Navier-Stokes equation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic characteristic","subitem_subject_language":"en","subitem_subject_scheme":"Other"}]},"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":"CASPERを用いたONERA M5形態まわりの流れ解析","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"CASPERを用いたONERA M5形態まわりの流れ解析"}]},"item_type_id":"5","owner":"1","path":["1891","1915"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"38058","relation_version_is_last":true,"title":["CASPERを用いたONERA M5形態まわりの流れ解析"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T22:45:49.396001+00:00"}