Stall control with feathers : self-activated flaps on finite wings at low Reynolds numbers

We present experimental data on the use of a “pop-up feather” type high lift device (passive flap) on the upper side of the wing. While a number of previous studies have shown the effectiveness of this flap in two-dimensional geometries, we focus here on the use of the flap on finite wings and th...

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Bibliographic Details
Main Authors: Wang, C.H. John., Schlüter, Jörg.
Other Authors: School of Mechanical and Aerospace Engineering
Format: Article
Language:English
Published: 2013
Online Access:https://hdl.handle.net/10356/85663
http://hdl.handle.net/10220/13076
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Institution: Nanyang Technological University
Language: English
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