{"created":"2023-06-20T14:39:15.033911+00:00","id":5963,"links":{},"metadata":{"_buckets":{"deposit":"dfb3f904-19ff-4c31-af43-ec06d04eeb91"},"_deposit":{"created_by":1,"id":"5963","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"5963"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00005963","sets":["1887:1891","9:789:998:1024"]},"author_link":["29553","29555","29558","29559","29554","29557","29556","29560"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Aerodynamic design of supersonic biplane: Current status and future direction"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2006-12-01","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"106","bibliographicPageStart":"101","bibliographicVolumeNumber":"JAXA-SP-06-010","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構特別資料: 航空宇宙数値シミュレーション技術シンポジウム2006論文集"},{"bibliographic_title":"JAXA Special Publication: Proceedings of Aerospace Numerical Simulation Symposium 2006","bibliographic_titleLang":"en"}]}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Nowadays, the development of Supersonic Transport (SST) is attracting international attention again. However, in supersonic flights, we face the problem of 'sonic boom', which is induced by a shock wave. To alleviate the problem of sonic boom, the idea of reducing shock wave using Busemann biplane has been proposed. The interaction of shock waves between the two wings cancels out or reduces the shock waves created by individual wings. This research discusses two issues about Busemann biplane. One is the unstarted condition during acceleration. The other is the three-dimensional configuration of Busemann biplane. Unstarted condition happens due to the unsatisfied condition with Kantrowitz Donaldson Criteria. Unstarted condition that holds in the criteria is confirmed by analyzing accelerate phenomenon using Computational Fluid Dynamics (CFD) analysis. The other important issue is that the shock front should be planar to cancel out the shock waves between two wings. The caret wing induces a planar shock front. Three caret wing configurations are analyzed to examine how the planar shock front are created using CFD analysis.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0063154019","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-06-010","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"}]},"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":"東北大学流体科学研究所"},{"subitem_text_value":"東北大学流体科学研究所"},{"subitem_text_value":"東北大学流体科学研究所"},{"subitem_text_value":"東北大学"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"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"},{"subitem_text_language":"en","subitem_text_value":"Institute of Fluid Science, Tohoku University"},{"subitem_text_language":"en","subitem_text_value":"Tohoku University"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"米澤, 誠仁"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"山下, 博"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"大林, 茂"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"楠瀬, 一洋"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yonezawa, Masahito","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yamashita, Hiroshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Obayashi, Shigeru","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kusunose, Kazuhiro","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":"63154019.pdf","filesize":[{"value":"1.4 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"63154019.pdf","url":"https://jaxa.repo.nii.ac.jp/record/5963/files/63154019.pdf"},"version_id":"fc259387-f23a-449e-86dc-2c50d5f6dc75"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"超音速翼","subitem_subject_scheme":"Other"},{"subitem_subject":"Busemann複葉機","subitem_subject_scheme":"Other"},{"subitem_subject":"超音速複葉機","subitem_subject_scheme":"Other"},{"subitem_subject":"チョーク流れ","subitem_subject_scheme":"Other"},{"subitem_subject":"衝撃波","subitem_subject_scheme":"Other"},{"subitem_subject":"圧力分布","subitem_subject_scheme":"Other"},{"subitem_subject":"超音速輸送機","subitem_subject_scheme":"Other"},{"subitem_subject":"計算流体力学","subitem_subject_scheme":"Other"},{"subitem_subject":"マッハ数","subitem_subject_scheme":"Other"},{"subitem_subject":"抗力","subitem_subject_scheme":"Other"},{"subitem_subject":"インテークディフューザ","subitem_subject_scheme":"Other"},{"subitem_subject":"不始動条件","subitem_subject_scheme":"Other"},{"subitem_subject":"supersonic airfoil","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Busemann biplane","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"supersonic biplane","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"choked flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"shock wave","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"pressure distribution","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"supersonic transport","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"computational fluid dynamics","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Mach number","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"drag","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"intake diffuser","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"unstart condition","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":"複葉超音速翼空力設計の現状と課題","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"複葉超音速翼空力設計の現状と課題"}]},"item_type_id":"5","owner":"1","path":["1024","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"5963","relation_version_is_last":true,"title":["複葉超音速翼空力設計の現状と課題"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T08:05:11.891901+00:00"}