{"created":"2023-06-20T14:39:07.733582+00:00","id":5804,"links":{},"metadata":{"_buckets":{"deposit":"348755a0-5a24-4c1a-98d1-e23f2701b4df"},"_deposit":{"created_by":1,"id":"5804","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"5804"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00005804","sets":["1887:1891","9:789:998:1005"]},"author_link":["477131","477137","477139","477141","477132","477138","477140","477129","477136","477142","477130","477135","477134","477133"],"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2007-03-30","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"671","bibliographicPageStart":"658","bibliographicVolumeNumber":"JAXA-SP-06-029E","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 International Workshops on Numerical Simulation Technology for Design of Next Generation Supersonic Civil Transport (SST-CFD Workshop)","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":"SST-CFDワークショップ.次世代超音速機の数値シミュレーション利用技術に関する国際ワークショップ: Toward the Future form NEXST-1 Flight Trial 宇宙航空研究開発機構 20061012-20061013 東京 日本","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":"SST-CFD Workshop. International Workshops on Numerical Simulation Technology for Design of Next Generation Supersonic Civil Transport: Toward the Future form NEXST-1 Flight Trial Japan Aerospace Exploration Agency 20061012-20061013 Tokyo Japan","subitem_description_type":"Other"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"CFD (Computational Fluid Dynamics) analyses of a flow field around supersonic transport, NEXST-1 (National EXperimental Supersonic Transport-1) are conducted. The CFD results are compared with flight test data. In this paper, C(sub D) and C(sub p) discrepancies between them are mainly discussed with consideration of the effects of transition and local geometry change by protuberances of measuring instruments. As for the C(sub D) discrepancies, CFD results have more (4-9 cts) profile drag, which could be the sum of spurious numerical error and turbulence model mismatch. As for the C(sub p) discrepancies, C(sub p) values at local points are definitely influenced by protuberances. Through the discussion, we also demonstrate how the CFD simulation can augment the validity of the flight test data.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0063609073","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-06-029E","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"}]},"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":"東北大学 大学院工学研究科"},{"subitem_text_value":"三菱重工業"},{"subitem_text_value":"三菱重工業"},{"subitem_text_value":"東北大学 大学院工学研究科"},{"subitem_text_value":"東北大学 大学院工学研究科"},{"subitem_text_value":"東北大学 大学院工学研究科"},{"subitem_text_value":"東北大学 大学院工学研究科"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Tohoku University Graduate School of Engineering"},{"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":"Tohoku University Graduate School of Engineering"},{"subitem_text_language":"en","subitem_text_value":"Tohoku University Graduate School of Engineering"},{"subitem_text_language":"en","subitem_text_value":"Tohoku University Graduate School of Engineering"},{"subitem_text_language":"en","subitem_text_value":"Tohoku University Graduate School of Engineering"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"梅田, 成紀"}],"nameIdentifiers":[{"nameIdentifier":"477129","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"竹中, 啓三"}],"nameIdentifiers":[{"nameIdentifier":"477130","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"畑中, 圭太"}],"nameIdentifiers":[{"nameIdentifier":"477131","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"平山, 大介"}],"nameIdentifiers":[{"nameIdentifier":"477132","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"山崎, 渉"}],"nameIdentifiers":[{"nameIdentifier":"477133","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"松島, 紀佐"}],"nameIdentifiers":[{"nameIdentifier":"477134","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"中橋, 和博"}],"nameIdentifiers":[{"nameIdentifier":"477135","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Umeda, Masaki","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"477136","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Takenaka, Keizo","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"477137","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Hatanaka, Keita","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"477138","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Hirayama, Daisuke","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"477139","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Yamazaki, Wataru","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"477140","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Matsushima, Kisa","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"477141","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Nakahashi, Kazuhiro","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"477142","nameIdentifierScheme":"WEKO"}]}]},"item_files":{"attribute_name":"ファイル情報","attribute_type":"file","attribute_value_mlt":[{"accessrole":"open_date","date":[{"dateType":"Available","dateValue":"2020-02-10"}],"displaytype":"detail","filename":"63609073.pdf","filesize":[{"value":"9.5 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"63609073.pdf","url":"https://jaxa.repo.nii.ac.jp/record/5804/files/63609073.pdf"},"version_id":"8443d9f0-e506-47f1-b6d4-b59d0fac0c3a"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"超音速機","subitem_subject_scheme":"Other"},{"subitem_subject":"航空機設計","subitem_subject_scheme":"Other"},{"subitem_subject":"NEXST-1","subitem_subject_scheme":"Other"},{"subitem_subject":"計算流体力学","subitem_subject_scheme":"Other"},{"subitem_subject":"流れの分布","subitem_subject_scheme":"Other"},{"subitem_subject":"隆起","subitem_subject_scheme":"Other"},{"subitem_subject":"層流翼型","subitem_subject_scheme":"Other"},{"subitem_subject":"抗力低減","subitem_subject_scheme":"Other"},{"subitem_subject":"揚抗比","subitem_subject_scheme":"Other"},{"subitem_subject":"乱流モデル","subitem_subject_scheme":"Other"},{"subitem_subject":"格子生成","subitem_subject_scheme":"Other"},{"subitem_subject":"飛行試験","subitem_subject_scheme":"Other"},{"subitem_subject":"supersonic aircraft","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aircraft design","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"NEXST-1","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"computational fluid dynamics","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flow distribution","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"protuberance","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"laminar flow airfoil","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"drag reduction","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"lift drag ratio","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"turbulence model","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"grid generation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flight test","subitem_subject_language":"en","subitem_subject_scheme":"Other"}]},"item_language":{"attribute_name":"言語","attribute_value_mlt":[{"subitem_language":"eng"}]},"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":"Validation of CFD capability for supersonic transport analysis using NEXST-1 flight test results","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Validation of CFD capability for supersonic transport analysis using NEXST-1 flight test results","subitem_title_language":"en"}]},"item_type_id":"5","owner":"1","path":["1005","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"5804","relation_version_is_last":true,"title":["Validation of CFD capability for supersonic transport analysis using NEXST-1 flight test results"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:33:14.573618+00:00"}