High-Lift Capability of Low Aspect Ratio Wings Utilizing Circulation Control and Upper Surface Blowing

1980 ◽  
Author(s):  
Roger J. Furey
Keyword(s):  
Aspect Ratio ◽  
Circulation Control ◽  
High Lift ◽  
Low Aspect Ratio ◽  
Low Aspect Ratio Wings

Design of high-lift airfoils for low aspect ratio wings with endplates

1997 ◽  
Author(s):  
Ashok Gopalarathnam ◽  
Michael Selig ◽  
Frank Hsu ◽  
Ashok Gopalarathnam ◽  
Michael Selig ◽  
...  
Keyword(s):  
Aspect Ratio ◽  
High Lift ◽  
Low Aspect Ratio ◽  
Low Aspect Ratio Wings

Passive mitigation of roll stall for low aspect ratio wings

2013 ◽  
Vol 27 (9) ◽  
pp. 667-681 ◽  
Author(s):  
Matt Shields ◽  
Kamran Mohseni
Keyword(s):  
Aspect Ratio ◽  
Low Aspect Ratio ◽  
Low Aspect Ratio Wings

Leading Edge and Wing Tip Flow Control on Low Aspect Ratio Wings

2010 ◽  
Author(s):  
Stefan Vey ◽  
David Greenblatt ◽  
Christian Nayeri ◽  
Christian Paschereit
Keyword(s):  
Aspect Ratio ◽  
Flow Control ◽  
Leading Edge ◽  
Low Aspect Ratio ◽  
Wing Tip ◽  
Low Aspect Ratio Wings

scholarly journals On the lift-optimal aspect ratio of a revolving wing at low Reynolds number

2018 ◽  
Vol 15 (143) ◽  
pp. 20170933 ◽  
Author(s):  
T. Jardin ◽  
T. Colonius
Keyword(s):  
Aspect Ratio ◽  
Lift Coefficient ◽  
Leading Edge ◽  
Rossby Number ◽  
Subsequent Work ◽  
High Lift ◽  
Low Aspect Ratio ◽  
Axis Of Rotation ◽  
Edge Vortex ◽  
Convergent Solution

Lentink & Dickinson (2009 J. Exp. Biol. 212 , 2705–2719. ( doi:10.1242/jeb.022269 )) showed that rotational acceleration stabilized the leading-edge vortex on revolving, low aspect ratio (AR) wings and hypothesized that a Rossby number of around 3, which is achieved during each half-stroke for a variety of hovering insects, seeds and birds, represents a convergent high-lift solution across a range of scales in nature. Subsequent work has verified that, in particular, the Coriolis acceleration plays a key role in LEV stabilization. Implicit in these results is that there exists an optimal AR for wings revolving about their root, because it is otherwise unclear why, apart from possible morphological reasons, the convergent solution would not occur for an even lower Rossby number. We perform direct numerical simulations of the flow past revolving wings where we vary the AR and Rossby numbers independently by displacing the wing root from the axis of rotation. We show that the optimal lift coefficient represents a compromise between competing trends with competing time scales where the coefficient of lift increases monotonically with AR, holding Rossby number constant, but decreases monotonically with Rossby number, when holding AR constant. For wings revolving about their root, this favours wings of AR between 3 and 4.

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