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複素特性曲線法を用いた超音速自然層流翼の遷移解析
https://jaxa.repo.nii.ac.jp/records/21692
https://jaxa.repo.nii.ac.jp/records/21692ecb2f168-ae7a-4d23-b968-109b5350fba2
Item type | 学術雑誌論文 / Journal Article(1) | |||||
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公開日 | 2016-03-28 | |||||
タイトル | ||||||
タイトル | 複素特性曲線法を用いた超音速自然層流翼の遷移解析 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Complex Ray Theory | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | 3-D Supersonic Boundary Layers | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Transition Prediction | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Eigenvalue Analysis | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Parabolized Stability Equations | |||||
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 | Transition Analysis with Complex Ray Theory for Supersonic Natural Laminar Flow Wing | |||||
著者 |
井手, 優紀
× 井手, 優紀× 吉田, 憲司× 上田, 良稲× Ide, Yuki× Yoshida, Kenji× Ueda, Yoshine |
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出版者 | ||||||
出版者 | Japan Society for Aeronautical and Space Sciences | |||||
出版者(英) | ||||||
出版者 | 日本航空宇宙学会 | |||||
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 64, 号 1, p. 71(71)-78(78), 発行日 2016-02-05 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | We applied a method based on Complex-ray theory (CRT) to the stability analysis of three-dimensional boundary layers at supersonic flight test conditions of the JAXA's experimental airplane called, NEXST-1, and investigated its capability. The dispersion relation was numerically obtained by the eigenvalue equations and linear parabolized stability equations (PSE). By adapting two kinematic wave theoretical models, we found out which wave type was dominant at measured transition locations of the flight test in 2005. As a result, it has been found that the dominant wave type on the outer wing section of the NEXST-1 was wedge-shaped disturbance, on the other hand, it was two dimensional wave-packets on the inner wing section. From the view point of transition prediction using an e to the Nth power method, there was no difference of transition N factors (N(sub tr)) between the results by the eigenvalue solutions with and without CRT method. Only a use of PSE with CRT, however, was able to reduce the discrepancy of N(sub tr). among cross sections, owing to the nonparallel effect of flows. | |||||
内容記述 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 形態: 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 illustrations | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 1344-6460 | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA11307372 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: DS1540529011 |