Wake Vortex Control Using Rapidly Actuated Segmented Gurney Flaps

Author(s):  
Claude Matalanis ◽  
John Eaton
AIAA Journal ◽  
2007 ◽  
Vol 45 (2) ◽  
pp. 321-328 ◽  
Author(s):  
Claude G. Matalanis ◽  
John K. Eaton

2012 ◽  
Vol 56 (01) ◽  
pp. 12-22
Author(s):  
Liu Zhihua ◽  
Xiong Ying ◽  
Tu Chengxu

The submarine propeller works in the submarine wake with severe circumferential nonuniformity, which causes the hydrodynamic force to act on the blade. This results in severe oscillation with the rotation of the propeller and impairs the hydrodynamics and noise performance of the submarine propeller. The horseshoe vortex generated at the hull-appendages junctions of the submarine has important influence on wake uniformity. In the present study, the state of the submarine horseshoe vortex is analyzed and a new method of vortex control baffler is presented. The aim is to weaken the horseshoe vortex. Based on the wind tunnel experiment and numerical simulation on the submarine model, the vortex control baffler can decrease the strength of the submarine horseshoe vortex and improve the uniformity of the submarine wake. Vortex control bafflers adapted for the fully appended SUBOFF model are designed, and the unsteady force of three kinds of propellers functioned after the SUBOFF model is calculated numerically. The results show that although the skew angle and blade number are different, the amplitudes of the unsteady force acting on the blades of all three propellers decreased by 50% to 80% due to the effects of the vortex control baffler.


2004 ◽  
Vol 16 (2) ◽  
pp. 452-456 ◽  
Author(s):  
D. R. Arcas ◽  
L. G. Redekopp
Keyword(s):  

AIAA Journal ◽  
2007 ◽  
Vol 45 (8) ◽  
pp. 1874-1884 ◽  
Author(s):  
Claude G. Matalanis ◽  
John K. Eaton
Keyword(s):  

Author(s):  
Thomas McLaughlin ◽  
Matthew Munska ◽  
Joseph Vaeth ◽  
Travis Dauwalter ◽  
Jeffrey Goode ◽  
...  

2013 ◽  
Vol 365-366 ◽  
pp. 827-834
Author(s):  
Yi He ◽  
Jin Wen Yang ◽  
Feng Bao

The present paper is on the experimental investigation of a potentially effective method to alleviate the strength of aircraft wake vortex. The research work was carried out in a water-towing tank which equipped with a 2-D PIV system. By using modified flaps attached to the baseline-airfoil, the Rayleigh-Ludwieg instability of the wake vortex was activated, resulting in a premature dissipation of the wake vortex. The experimental results of PIV measurement exhibited that the circulation of the wake vortex was reduced to over 50% for the optimal case at 45 wingspans downstream with suitable settings, which proved the effectiveness of the modified-flap treatment in alleviating the wake vortex under labor conditions.


2009 ◽  
Vol 16 (2) ◽  
pp. 103-125 ◽  
Author(s):  
Robert C. Nelson ◽  
Brian M. Babie
Keyword(s):  

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