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衝撃波の相殺効果を利用した複葉超音速翼型の研究
http://hdl.handle.net/10110/00018896
http://hdl.handle.net/10110/00018896081d6936-c968-490c-89d4-cf5832376bb8
名前 / ファイル | ライセンス | アクション |
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NihonKokuUchuGakkai_55_636_001to007_Matsushima (1.2 MB)
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Item type | 学術雑誌論文 / Journal Article(1) | |||||
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公開日 | 2018-08-21 | |||||
タイトル | ||||||
タイトル | 衝撃波の相殺効果を利用した複葉超音速翼型の研究 | |||||
タイトル | ||||||
言語 | en | |||||
タイトル | A Study in the Supersonic Biplane Utilizing Its Shock Wave Cancellation Effect | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | Supersonic | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | Busemann Biplane | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | Shockwave Cancellation & Reduction | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | Inverse Problems | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | CFD | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | Computational Fluid Dynamics | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | Supersonic | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | Busemann Biplane | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | Shockwave Cancellation & Reduction | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | Inverse Problems | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | CFD | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | Computational Fluid Dynamics | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_6501 | |||||
資源タイプ | journal article | |||||
著者 |
楠瀬, 一洋
× 楠瀬, 一洋× 松島, 紀佐× 後藤, 悠一郎× 丸山, 大悟× 山下, 博× 米澤, 誠仁 |
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著者別名 | ||||||
姓名 | Kusunose, Kazuhiro | |||||
著者別名 | ||||||
姓名 | Matsushima, Kisa | |||||
著者別名 | ||||||
姓名 | Goto, Yuichiro | |||||
著者別名 | ||||||
姓名 | Maruyama, Daigo | |||||
著者別名 | ||||||
姓名 | Yamashita, Hiroshi | |||||
著者別名 | ||||||
姓名 | Yonezawa, Masahito | |||||
その他(別言語等)のタイトル | ||||||
その他のタイトル | A Study in the Supersonic Biplane Utilizing Its Shock Wave Cancellation Effect | |||||
抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | One of the fundamental problems preventing commercial transport aircraft from supersonic flight is the creation of strong shock waves. Here, a biplane concept is proposed that will enable a significant reduction of shock waves: Introduce a second wing nearly parallel to the conventional wing, creating a biplane configuration. The interaction between the two wings will cancel or reduce the shock waves created by the individual wings. Several simple two-dimensional biplane configurations are currently under study, using CFD (computational fluid dynamics) codes, Euler calculations for inviscid flow analysis and inverse-problem analysis for wing design, to demonstrate our biplane concept. | |||||
引用 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 日本航空宇宙学会論文集=JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES 55(636), 1-7.(2007) | |||||
書誌情報 |
日本航空宇宙学会論文集 en : JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES 巻 55, 号 636, p. 1-7, 発行日 2007 |
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ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 13446460 | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA11307372 | |||||
DOI | ||||||
関連タイプ | isIdenticalTo | |||||
識別子タイプ | DOI | |||||
関連識別子 | 10.2322/jjsass.55.1 | |||||
権利 | ||||||
権利情報 | Copyright 2007 The Japan Society for Aeronautical and Space Sciences. | |||||
フォーマット | ||||||
内容記述タイプ | Other | |||||
内容記述 | application/pdf | |||||
著者版フラグ | ||||||
出版タイプ | VoR | |||||
出版タイプResource | http://purl.org/coar/version/c_970fb48d4fbd8a85 | |||||
論文ID(NAID) | ||||||
関連タイプ | isIdenticalTo | |||||
識別子タイプ | NAID | |||||
関連識別子 | 130000147077 | |||||
出版者 | ||||||
出版者 | 一般社団法人 日本航空宇宙学会 | |||||
出版者 | ||||||
出版者 | THE JAPAN SOCIETY AERONAUTICAL AND SPACE SCIENCES | |||||
資源タイプ(DSpace) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Article |