Abstract
In this study, experimental investigations were made regarding the effect of riblets on the streak instability in boundary layer. The streak instability is now regarded as a major source of the self-regeneration mechanism for the hairpin type coherent structures in turbulent boundary layer flow. Thus, it is important to control the instability to suppress the drag-inducing vortical structure in terms of drag reduction. Toward enhancing the measurement accuracy and spatial resolution, an enlarged version of riblets was applied to a streak which was artificially induced by a microwing in a laminar boundary layer. It is found that the riblets have attenuation effect on the streak instability, i.e., to reduce the spanwise velocity gradient of the quasi-streamwise streak in boundary layer.
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Abbreviations
- U0 :
-
Freestream velocity
- u′:
-
Turbulence intensity
- x 0 :
-
Location of the microwing/roughness elements in the streamwise coordinate
- y 0 :
-
Location of the microwing/roughness elements in the wall-normal coordinate
- δ* :
-
Displacement thickness of the boundary layer
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Boiko, A.V., Jung, K.H., Chun, H.H. et al. Effect of riblets on the streaky structures excited by free stream tip vortices in boundary layer. J Mech Sci Technol 21, 196–206 (2007). https://doi.org/10.1007/BF03161725
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DOI: https://doi.org/10.1007/BF03161725