Application of vortex identification schemes to direct numerical simulation data of a transitional boundary layer

2013 ◽  
Vol 25 (1) ◽  
pp. 015102 ◽  
Author(s):  
Brian Pierce ◽  
Parviz Moin ◽  
Taraneh Sayadi
Keyword(s):  
Numerical Simulation ◽  
Boundary Layer ◽  
Direct Numerical Simulation ◽  
Vortex Identification ◽  
Simulation Data ◽  
Direct Numerical Simulation Data ◽  
Identification Schemes ◽  
Transitional Boundary Layer

Analysis of shock motion in shockwave and turbulent boundary layer interaction using direct numerical simulation data

2007 ◽  
Vol 594 ◽  
pp. 71-83 ◽  
Author(s):  
MINWEI WU ◽  
M. PINO MARTÍN
Keyword(s):  
Numerical Simulation ◽  
Boundary Layer ◽  
Direct Numerical Simulation ◽  
Low Frequency ◽  
Separation Point ◽  
Online Version ◽  
Simulation Data ◽  
Direct Numerical Simulation Data ◽  
Shock Motion ◽  
Shock Location

Direct numerical simulation data of a Mach 2.9, 24○ compression ramp configuration are used to analyse the shock motion. The motion can be observed from the animated DNS data available with the online version of the paper and from wall-pressure and mass-flux signals measured in the free stream. The characteristic low frequency is in the range of (0.007–0.013) U∞/δ, as found previously. The shock motion also exhibits high-frequency, of O(U∞/δ), small-amplitude spanwise wrinkling, which is mainly caused by the spanwise non-uniformity of turbulent structures in the incoming boundary layer. In studying the low-frequency streamwise oscillation, conditional statistics show that there is no significant difference in the properties of the incoming boundary layer when the shock location is upstream or downstream. The spanwise-mean separation point also undergoes a low-frequency motion and is found to be highly correlated with the shock motion. A small correlation is found between the low-momentum structures in the incoming boundary layer and the separation point. Correlations among the spanwise-mean separation point, reattachment point and the shock location indicate that the low-frequency shock unsteadiness is influenced by the downstream flow. Movies are available with the online version of the paper.

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