Wake Vortex Field of an Airfoil Equipped with an Active Finite Gurney Flap

Author(s):  
Alena B. Bach ◽  
Georgios Pechlivanoglou ◽  
C. Nayeri ◽  
Christian O. Paschereit
Keyword(s):  
2006 ◽  
Vol 43 (5) ◽  
pp. 1555-1558 ◽  
Author(s):  
Vojin R. Nikolic
Keyword(s):  

2021 ◽  
Vol 2021 ◽  
pp. 1-10
Author(s):  
Xin He ◽  
Yilong Ma ◽  
Hong Yang ◽  
Yaqing Chen

In order to relieve the stress caused by the surge of flight flow, Closely Spaced Parallel Runways (CSPRs) have been built in many hub airports, and a paired approach mode has been applied to CSPRs in some countries. This paper proposes a method for optimizing the wake separation between aircrafts which utilizes a paired approach, aiming at reducing longitudinal separation by using computational fluid dynamics technology. Firstly, the model of the wake vortex field of the paired lead aircraft is constructed. Secondly, the numerical simulation preparation for the characteristics of the wake vortex field is completed through the computational pretreatment of the model. Thirdly, a calculation model of wake safety interval based on paired approach operation is established. Finally, the proposed method shows its superiority comparing with other methods. This method realized visual analysis of wake vortex through optimization modeling based on computational fluid dynamics, contributing to increasing the capacity of the runway and improving the operation efficiency of an aerodrome.


2007 ◽  
Vol 44 (4) ◽  
pp. 1398-1402 ◽  
Author(s):  
T. Lee ◽  
L. Lee

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

AIAA Journal ◽  
2000 ◽  
Vol 38 ◽  
pp. 643-656 ◽  
Author(s):  
Jongil Han ◽  
Yuh-Lang Lin ◽  
S. P. Arya ◽  
Fred H. Proctor

AIAA Journal ◽  
1997 ◽  
Vol 35 ◽  
pp. 1888-1890 ◽  
Author(s):  
Philippe Giguere ◽  
Guy Dumas ◽  
Jean Lemay

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