Study of Circulation Control Wing aerodynamics design

Autor:	Sasaki, Masafumi
Jazyk:	japonština
Rok vydání:	2008
Předmět:	2次元モデル validation 超臨界翼 空力設計 lift drag ratio 空力係数 angle of attack 揚抗比 high-lift device 計算流体力学 computational fluid dynamics trailing edge flap two dimensional model 風洞試験 aerodynamic design supercritical wing 実証 後縁フラップ aerodynamic coefficient 高揚力装置 迎角 航空機設計 wind tunnel test aircraft design
Zdroj:	宇宙航空研究開発機構特別資料: 第79回風洞研究会議論文集 = JAXA Special Publication: Proceedings of the Wind Tunnel Technology Association 79th Meeting. :33-36
ISSN:	1349-113X
Popis:	In this study, the aerodynamic performance of CCW (Circulation Control Wings) is investigated by two-dimensional (2D) CFD (Computational Fluid Dynamics) and the results are verified by 2D Wind-Tunnel-Test. It is found that CCW can achieve very higher lift and various lift-drag ratios at constant angle of attack (0 deg) in comparison with a conventional high-lift-device. 資料番号: AA0063897006 レポート番号: JAXA-SP-07-019
Databáze:	OpenAIRE
Externí odkaz:	https://explore.openaire.eu/search/publication?articleId=jairo_______::41d1849b66f172e25d91404fb94e8322 http://id.nii.ac.jp/1696/00005597/ Zobrazit plný text záznamu