Separated flow around an airfoil with a spoiler

When a spoiler is erected rapidly on the upper surface of a wing, it brings about a long-term reduction in lift and an increase in drag. However, it has a transient effect of increasing the lift (usually referred to as the adverse lift) on the wing due to the creation of a starting vortex shed from...

詳細記述

書誌詳細
第一著者: Xu, Cheng.
その他の著者: Yeung, William Wai Hung
フォーマット: 学位論文
言語:English
出版事項: 2009
主題:
オンライン・アクセス:http://hdl.handle.net/10356/19974