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...

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書目詳細資料
主要作者: Xu, Cheng.
其他作者: Yeung, William Wai Hung
格式: Theses and Dissertations
語言:English
出版: 2009
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在線閱讀:http://hdl.handle.net/10356/19974
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機構: Nanyang Technological University
語言: English