Direct Numerical Simulation of Laminar Boundary-Layer Separation and Separation Control on the Suction Side of an Airfoil at Low Reynolds Number Conditions

Author(s):  
Wolfgang Balzer ◽  
Hermann Fasel
2016 ◽  
Vol 29 (5) ◽  
pp. 1237-1246 ◽  
Author(s):  
Xin Zhang ◽  
Yong Huang ◽  
Xunnian Wang ◽  
Wanbo Wang ◽  
Kun Tang ◽  
...  

2008 ◽  
pp. 48-65

The constant C and the near-wall damping function f in the eddyviscosityrelation of the k-ε model are evaluated from direct numerical simulation (DNS) data for developed channel and boundary-layer flow, eachat two Reynolds numbers. Various existing


1975 ◽  
Vol 68 (4) ◽  
pp. 779-799 ◽  
Author(s):  
Vijay H. Arakeri

Flow visualization by the schlieren technique in the neighbourhood of a fully developed cavity on two axisymmetric headforms has shown the existence of laminar boundary-layer separation upstream of cavitation separation, and the distance between the two separations to be strongly dependent on Reynolds number. Based on present results, a semi-empirical method is developed to predict the position of cavitation separation on a smooth body. The method applies only in the Reynolds-number range when the cavitating body possesses laminar boundary-layer separation under non-cavitating conditions. Calculated positions of cavitation separation on a sphere by the method show good agreement with experimentally observed positions.


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