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正弦波変形による軸対称物体の超音速自然層流効果
https://jaxa.repo.nii.ac.jp/records/22620
https://jaxa.repo.nii.ac.jp/records/22620aa052aa1-c3ee-4a3d-8ecd-e05dea46ec75
Item type | 学術雑誌論文 / Journal Article(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2015-08-17 | |||||
タイトル | ||||||
タイトル | 正弦波変形による軸対称物体の超音速自然層流効果 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Drag Reduction | |||||
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 | Boundary-layer Transition | |||||
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 | Fuselage 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 | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Supersonic Natural Laminar Flow Effect on Axisymmetric Bodies with Sinusoidal Deformation | |||||
著者 |
徳川, 直子
× 徳川, 直子× 石川, 敬掲× 上田, 良稲× Tokugawa, Naoko× Ishikawa, Hiroaki× Ueda, Yoshine |
|||||
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 | ||||||
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 Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
TOUA Corporation | ||||||
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 | |||||
出版者(英) | ||||||
出版者 | The Japan Society for Aeronautical and Space Sciences | |||||
書誌情報 |
航空宇宙技術 巻 13, p. 55-59, 発行日 2014-08-28 |
|||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | The transition characteristics on candidate shapes were examined numerically and experimentally in order to design a natural laminar flow fuselage nose for supersonic transport. The candidate shapes were designed through axisymmetric sinusoidal deformations added on base shapes. Not only parameters of geometry which define the deformation, but also the conditions of uniform flow were varied to obtain the greatest effect of natural laminar flow. From the results, the natural laminar flow effect was found to be obtained in cases of the small ratio of pressure gradients in azimuthal and axial directions in the side area. The natural laminar flow effect was validated experimentally. | |||||
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 | 1884-0477 | |||||
DOI | ||||||
識別子タイプ | DOI | |||||
関連識別子 | http://dx.doi.org/10.2322/astj.13.55 | |||||
関連名称 | info:doi/10.2322/astj.13.55 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: PA1520035000 |