Internally mounted laser-Doppler-anemometry system for boundary layer measurement

2001 ◽  
Vol 30 (1) ◽  
pp. 111-114 ◽  
Author(s):  
D. Mouazé ◽  
P. M. Bélorgey
2018 ◽  
Vol 59 (5) ◽  
Author(s):  
Sophie Herpin ◽  
Laurent Perret ◽  
Romain Mathis ◽  
Christian Tanguy ◽  
Jean-Jacques Lasserre

2016 ◽  
Vol 139 (2) ◽  
Author(s):  
Christopher C. Beves ◽  
Tracie J. Barber

Dimples used as sub-boundary layer vortex generators have been shown to reduce wake size at large angles of incidence. The effect these dimples have on wingtip vortices with an endplate is measured via laser Doppler anemometry (LDA) on an inverted Tyrrell026 airfoil (ReC = 0.5 × 105 and chord = 0.075 m) in ground effect in order to determine the flow characteristics for this configuration and to see if previous measurements were performed in a thinner part of the wake due to any potential wake waviness. The strength of the wingtip vortex for the dimpled wing is 10% higher than the “clean” wing immediately downstream. The clean wing has large region of high turbulence throughout the wake, and the dimples reduce this by 50%. The net result is that dimples drastically improve the flow in the wake of the wing and endplate.


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