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Natural Laminar Flow Nose for Supersonic Transport Designed using Local Non-Axisymmetric Deformation
https://jaxa.repo.nii.ac.jp/records/22499
https://jaxa.repo.nii.ac.jp/records/224995ea80a8b-bb12-4a59-8703-84dc063f41fc
Item type | 学術雑誌論文 / Journal Article(1) | |||||
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公開日 | 2015-06-11 | |||||
タイトル | ||||||
言語 | en | |||||
タイトル | Natural Laminar Flow Nose for Supersonic Transport Designed using Local Non-Axisymmetric Deformation | |||||
言語 | ||||||
言語 | eng | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Supersonic | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Natural Laminar Flow | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Nose | |||||
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 | |||||
アクセス権 | ||||||
アクセス権 | metadata only access | |||||
アクセス権URI | http://purl.org/coar/access_right/c_14cb | |||||
著者 |
徳川, 直子
× 徳川, 直子× 石川, 敬掲× 戸塚, 絢子× 上田, 良稲× Tokugawa, Naoko× Ishikawa, Hiroaki× Tozuka, Ayako× Ueda, Yoshine |
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著者所属 | ||||||
宇宙航空研究開発機構航空本部(JAXA) | ||||||
著者所属 | ||||||
株式会社TOUA | ||||||
著者所属 | ||||||
キヤノン | ||||||
著者所属 | ||||||
東京ビジネスサービス株式会社 | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Aeronautical Technology, Japan Aerospace Exploration Agenc (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
TOUA Co. Ltd | ||||||
著者所属(英) | ||||||
en | ||||||
Canon Inc. | ||||||
著者所属(英) | ||||||
en | ||||||
Tokyo Business Service Co. Ltd. | ||||||
出版者 | ||||||
出版者 | 日本航空宇宙学会(JSASS) | |||||
出版者(英) | ||||||
出版者 | The Japan Society for Aeronautical and Space Sciences (JSASS) | |||||
書誌情報 |
en : Transactions of the Japan Society for Aeronautical and Space Sciences, Aerospace Technology Japan 巻 12, p. 71-80, 発行日 2014 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | In order to design the natural laminar flow nose for the high Reynolds number condition suppressing the increase of pressure drag, “local” and “non-axisymmetric” deformation is applied to a base shape. Through the analysis for low Reynolds number cases, it is confirmed that the localized deformation suppresses the increase of pressure drag, and that non-axisymmetric deformation reduces pressure gradient in the azimuthal direction effectively in order to extend the laminar region. It is also shown that there is a capability of more extension of the natural laminar flow effect to the high Reynolds number condition corresponding to the real civil supersonic transport suppressing the increase of pressure drag. | |||||
内容記述 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 形態: カラー図版あり | |||||
内容記述(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Physical characteristics: Original contains color illustrations | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 1884-0485 | |||||
DOI | ||||||
識別子タイプ | DOI | |||||
関連識別子 | http://dx.doi.org/10.2322/tastj.12.71 | |||||
関連名称 | info:doi/10.2322/tastj.12.71 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: PA1420055000 |