{"created":"2024-02-22T10:11:58.473808+00:00","id":2000318,"links":{},"metadata":{"_buckets":{"deposit":"15a4047d-f591-4391-aa02-38cbe033f887"},"_deposit":{"created_by":27,"id":"2000318","owners":[27],"pid":{"revision_id":0,"type":"depid","value":"2000318"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:02000318","sets":["1398:1530:1708577302544","1543:1874:1708591997170","1887:1891","9:789:1697171596136:1708575263412"]},"author_link":[],"item_1692869180903":{"attribute_name":"会議概要","attribute_value_mlt":[{"subitem_conference_country":"JPN","subitem_conference_date":{"subitem_conference_date_language":"ja","subitem_conference_period":"2023-07-12 - 2023-07-14"},"subitem_conference_names":[{"subitem_conference_name":"第55回流体力学講演会/第41回航空宇宙数値シミュレーション技術シンポジウム","subitem_conference_name_language":"ja"},{"subitem_conference_name":"The 55th Fluid Dynamics Conference / The 41st Aerospace Numerical Simulation Symposium","subitem_conference_name_language":"en"}],"subitem_conference_places":[{"subitem_conference_place":"東京","subitem_conference_place_language":"ja"},{"subitem_conference_place":"Tokyo","subitem_conference_place_language":"en"}],"subitem_conference_sponsors":[{"subitem_conference_sponsor":"航空宇宙数値シミュレーション技術シンポジウム運営委員会","subitem_conference_sponsor_language":"ja"}],"subitem_conference_venues":[{"subitem_conference_venue":"国立オリンピック記念青少年総合センター","subitem_conference_venue_language":"ja"},{"subitem_conference_venue":"National Olympics Memorial Youth Center","subitem_conference_venue_language":"en"}]}]},"item_1692929429513":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"One of the obstacles in realizing a supersonic passenger aircraft is the high operating cost due to poor fuel efficiency. Since frictional drag of aircraft significantly increases due to turbulent transition of the three-dimensional boundary layer, suppressing the transition (namely, laminarizing the flow) can be expected to reduce frictional drag and improve fuel efficiency. In this study, the laminar flow control is attempted by placing artificial sinusoidal roughness elements, SRE and its variant, near the leading edge. These roughness elements were applied to a supersonic Falkner-Skan-Cooke boundary layer (that is known as a three-dimensional boundary layer on flat plate), and the suppression effect of turbulent transition was verified by direct numerical simulation. The transition position was shifted backward at a sweep angle of 27 degrees, which was equivalent to that of a transonic wing.","subitem_description_language":"en","subitem_description_type":"Other"}]},"item_1692929640552":{"attribute_name":"内容記述","attribute_value_mlt":[{"subitem_description":"形態: カラー図版あり","subitem_description_language":"ja","subitem_description_type":"Other"},{"subitem_description":"Physical  characteristics: Original contains color illustrations","subitem_description_language":"en","subitem_description_type":"Other"}]},"item_1693474141533":{"attribute_name":"資料番号(Local)","attribute_value_mlt":[{"subitem_relation_type_id":{"subitem_relation_type_id_text":"資料番号: AA2330026014","subitem_relation_type_select":"Local"}}]},"item_1695282775758":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_language":"ja","subitem_text_value":"東北大学大学院工学研究科 : 東北大学流体科学研究所"},{"subitem_text_language":"ja","subitem_text_value":"東北大学流体科学研究所"},{"subitem_text_language":"ja","subitem_text_value":"東北大学流体科学研究所"},{"subitem_text_language":"en","subitem_text_value":"Graduate School of Engineering, Tohoku University : Institute of Fluid Science, Tohoku University"},{"subitem_text_language":"en","subitem_text_value":"Institute of Fluid Science, Tohoku University"},{"subitem_text_language":"en","subitem_text_value":"Institute of Fluid Science, Tohoku University"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2024-02-27","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"255","bibliographicPageStart":"245","bibliographicVolumeNumber":"JAXA-SP-23-009","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構特別資料: 第55回流体力学講演会/第41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_titleLang":"ja"},{"bibliographic_title":"JAXA Special Publication: Proceedings of the 55th Fluid Dynamics Conference / the 41st Aerospace Numerical Simulation Symposium","bibliographic_titleLang":"en"}]}]},"item_3_description_33":{"attribute_name":"レポート番号","attribute_value_mlt":[{"subitem_description":"レポート番号: JAXA-SP-23-009","subitem_description_language":"ja","subitem_description_type":"Other"}]},"item_3_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙航空研究開発機構 (JAXA)","subitem_publisher_language":"ja"},{"subitem_publisher":"Japan Aerospace Exploration Agency (JAXA)","subitem_publisher_language":"en"}]},"item_3_source_id_22":{"attribute_name":"ISSN ONLINE","attribute_value_mlt":[{"subitem_source_identifier":"2433-2232","subitem_source_identifier_type":"EISSN"}]},"item_3_version_type_30":{"attribute_name":"著者版フラグ","attribute_value_mlt":[{"subitem_version_resource":"http://purl.org/coar/version/c_970fb48d4fbd8a85","subitem_version_type":"VoR"}]},"item_access_right":{"attribute_name":"アクセス権","attribute_value_mlt":[{"subitem_access_right":"open access","subitem_access_right_uri":"http://purl.org/coar/access_right/c_abf2"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorAffiliations":[{"affiliationNames":[{"affiliationName":"東北大学","affiliationNameLang":"ja"},{"affiliationName":"Tohoku University","affiliationNameLang":"en"}]}],"creatorNames":[{"creatorName":"庭野, 翔也","creatorNameLang":"ja"},{"creatorName":"NIWANO, Shoya","creatorNameLang":"en"}]},{"creatorAffiliations":[{"affiliationNames":[{"affiliationName":"東北大学","affiliationNameLang":"ja"},{"affiliationName":"Tohoku University","affiliationNameLang":"en"}]}],"creatorNames":[{"creatorName":"廣田, 真","creatorNameLang":"ja"},{"creatorName":"HIROTA, Makoto","creatorNameLang":"en"}]},{"creatorAffiliations":[{"affiliationNames":[{"affiliationName":"東北大学","affiliationNameLang":"ja"},{"affiliationName":"Tohoku University","affiliationNameLang":"en"}]}],"creatorNames":[{"creatorName":"大林, 茂","creatorNameLang":"ja"},{"creatorName":"OBAYASHI, Shigeru","creatorNameLang":"en"}]}]},"item_files":{"attribute_name":"ファイル情報","attribute_type":"file","attribute_value_mlt":[{"accessrole":"open_date","date":[{"dateType":"Available","dateValue":"2024-02-27"}],"filename":"AA2330026014.pdf","format":"application/pdf","mimetype":"application/pdf","url":{"url":"https://jaxa.repo.nii.ac.jp/record/2000318/files/AA2330026014.pdf"},"version_id":"6676ec8b-16d9-4f1b-8bc5-6f3e8acc64d1"}]},"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":"超音速三次元境界層流れへの波形粗さの適用による層流化効果の数値的検証","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"超音速三次元境界層流れへの波形粗さの適用による層流化効果の数値的検証","subitem_title_language":"ja"},{"subitem_title":"Numerical verification of the laminarization effect of applying sinusoidal roughness to supersonic three-dimensional boundary layer flow","subitem_title_language":"en"}]},"item_type_id":"40003","owner":"27","path":["1708575263412","1891","1708577302544","1708591997170"],"pubdate":{"attribute_name":"PubDate","attribute_value":"2024-02-27"},"publish_date":"2024-02-27","publish_status":"0","recid":"2000318","relation_version_is_last":true,"title":["超音速三次元境界層流れへの波形粗さの適用による層流化効果の数値的検証"],"weko_creator_id":"27","weko_shared_id":-1},"updated":"2024-02-27T04:31:41.731896+00:00"}