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Initial growth of a disturbance in a boundary layer influenced by a circular cylinder wake

Published online by Cambridge University Press:  08 February 2013

Guosheng He
Affiliation:
Fluid Mechanics Key Laboratory of Education Ministry, Beijing University of Aeronautics and Astronautics, 100191 Beijing, P.R. China
Jinjun Wang*
Affiliation:
Fluid Mechanics Key Laboratory of Education Ministry, Beijing University of Aeronautics and Astronautics, 100191 Beijing, P.R. China
Chong Pan
Affiliation:
Fluid Mechanics Key Laboratory of Education Ministry, Beijing University of Aeronautics and Astronautics, 100191 Beijing, P.R. China
*
Email address for correspondence: jjwang@buaa.edu.cn

Abstract

The initial growth of a disturbance induced by a near-wall circular cylinder in a flat-plate boundary layer is experimentally investigated using both particle image velocimetry and hydrogen bubble visualization techniques. The secondary spanwise vortices appear in the near-wall region as a direct response to the outside passing wake vortices, consistent with previous studies on similar models (Pan et al., J. Fluid Mech., vol. 603, 2008, pp. 367–389; Mandal & Dey, J. Fluid Mech., vol. 684, 2011, pp. 60–84). The streamwise variation of the total disturbance energy within the boundary layer shows a two-stage growth, which characterizes the initial transition process: the first exponential growth stage, followed by a region with slower growth rate. It is revealed that these two stages of growth are related to the formation and the destabilization of the secondary vortex in the near-wall region. The technique of dynamic mode decomposition is used to decompose the total disturbance into temporally orthogonalized modes, and it shows that the first growth stage largely results from the increased disturbance at the same frequency as that of the wake vortex shedding, while the second growth stage comprises the disturbance growth in a number of frequencies, especially the lower ones.

Type
Papers
Copyright
©2013 Cambridge University Press

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References

Adrian, R. J., Christensen, K. T. & Liu, Z. C. 2000 Analysis and interpretation of instantaneous turbulent velocity fields. Exp. Fluids 29 (3), 275290.CrossRefGoogle Scholar
Andersson, P., Berggren, M. & Henningson, D. S. 1999 Optimal disturbances and bypass transition in boundary layers. Phys. Fluids 11, 134150.CrossRefGoogle Scholar
Chen, K. K., Tu, J. H. & Rowley, C. W. 2012 Variants of dynamic mode decomposition: boundary condition, Koopman, and Fourier analyses. J. Nonlinear Sci., online.Google Scholar
Christensen, K. T. 2004 The influence of peak-locking errors on turbulence statistics computed from PIV ensembles. Exp. Fluids 36 (3), 484497.Google Scholar
Durbin, P. & Wu, X. H. 2007 Transition beneath vortical disturbances. Annu. Rev. Fluid Mech. 39, 107128.Google Scholar
Fransson, J. H. M., Matsubara, M. & Alfredsson, P. H. 2005 Transition induced by free stream turbulence. J. Fluid Mech. 527, 125.CrossRefGoogle Scholar
Hunt, J. C. R. & Durbin, P. A. 1999 Perturbed vortical layers and shear sheltering. Fluid Dyn. Res. 24, 375404.Google Scholar
Jacobs, R. G. & Durbin, P. A. 1998 Shear sheltering and the continuous spectrum of the orr-sommerfeld equation. Phys. Fluids 10, 20062011.Google Scholar
Jacobs, R. G. & Durbin, P. A. 2001 Simulations of bypass transition. J. Fluid Mech. 428, 185212.CrossRefGoogle Scholar
Kendall, J. M. 1985 Experimental study of disturbances produced in a pretransitional laminar boundary layer by weak free stream turbulence. AIAA Paper, 85-1695.Google Scholar
Kyriakides, N. K., Kastrinakis, E. G., Nychas, S. G. & Goulas, A. 1999 Aspects of flow structure during a cylinder wake-induced laminar/turbulent transition. AIAA J. 37, 11971205.CrossRefGoogle Scholar
Luchini, P. 2000 Reynolds-number-independent instability of the boundary layer over a flat surface: optimal perturbations. J. Fluid Mech. 404, 289309.Google Scholar
Mandal, A. C. & Dey, J. 2011 An experimental study of boundary layer transition induced by a cylinder wake. J. Fluid Mech. 684, 6084.CrossRefGoogle Scholar
Matsubara, M. & Alfredsson, P. H. 2001 Disturbance growth in boundary layers subjected to free stream turbulence. J. Fluid Mech. 430, 149168.CrossRefGoogle Scholar
Mayle, R. E. 1991 The role of laminar–turbulent transition in gas turbine engines. Trans. ASME: J. Turbomach. 113, 509537.Google Scholar
Morkovin, M. V. 1969 On the many faces of transition. In Viscous Drag Reduction (ed. Wells, C. S.), pp. 131. Plenum.Google Scholar
Ovchinnikov, V., Piomelli, U. & Choudhari, M. M. 2006 Numerical simulations of boundary-layer transition induced by a cylinder wake. J. Fluid Mech. 547, 413441.CrossRefGoogle Scholar
Pan, C., Wang, J. J. & He, G. S. 2012 Experimental investigation of wake-induced bypass transition control by surface roughness. Chin. Phys. Lett. 29 (10), 104704.Google Scholar
Pan, C., Wang, J. J., Zhang, P. F. & Feng, L. H. 2008 Coherent structures in bypass transition induced by a cylinder wake. J. Fluid Mech. 603, 367389.Google Scholar
Pan, C., Yu, D. S. & Wang, J. J. 2011 Dynamical mode decomposition of gurney flap wake flow. Theor. Appl. Mech. Lett. 1, 012002.Google Scholar
Price, S. J., Sumner, D., Smith, J. G., Leong, K. & Paidoussis, M. P. 2002 Flow visualization around a circular cylinder near to a plane wall. J. Fluids Struct. 16 (2), 175191.CrossRefGoogle Scholar
Rowley, C. W., Mezic, I., Bagheri, S., Schlatter, P. & Henningson, D. S. 2009 Spectral analysis of nonlinear flows. J. Fluid Mech. 641, 115127.Google Scholar
Sarkar, S. & Sarkar, S. 2009 Large-eddy simulation of wake and boundary layer interactions behind a circular cylinder. Trans. ASME: J. Fluids Engng 131 (9), 091201.Google Scholar
Scarano, F. & Riethmuller, M. L. 2000 Advances in iterative multigrid PIV image processing. Exp. Fluids 29, S51S60.CrossRefGoogle Scholar
Schmid, P. J. 2010 Dynamic mode decomposition of numerical and experimental data. J. Fluid Mech. 656, 528.CrossRefGoogle Scholar
Schrader, L. U., Brandt, L., Mavriplis, C. & Henningson, D. S. 2010 Receptivity to free stream vorticity of flow past a flat plate with elliptic leading edge. J. Fluid Mech. 653, 245271.CrossRefGoogle Scholar
Wang, J. J., Pan, C. & Zhang, P. F. 2009 On the instability and reproduction mechanism of a laminar streak. J. Turbul. 10 (26), 127.CrossRefGoogle Scholar
Wang, J. J., Zhang, C. & Pan, C. 2011 Effects of roughness elements on bypass transition induced by a circular cylinder wake. J. Vis. 14 (1), 5361.Google Scholar
Westerweel, J. 2000 Theoretical analysis of the measurement precision in particle image velocimetry. Exp. Fluids 29, S3S12.CrossRefGoogle Scholar
Westin, K. J. A., Boiko, A. V., Klingmann, B. G. B., Kozlov, V. V. & Alfredsson, P. H. 1994 Experiments in a boundary layer subjected to free stream turbulence. Part 1. Boundary layer structure and receptivity. J. Fluid Mech. 281, 193218.CrossRefGoogle Scholar
Wu, J., Pan, C. & Li, T. 2012 Experimental investigation on coherent structures at early stage of boundary layer bypass transition induced by wake impingement. Sci. China: Technol. Sci. 55 (11), 29812989.CrossRefGoogle Scholar
Zhang, C., Pan, C. & Wang, J. J. 2011 Evolution of vortex structure in boundary layer transition induced by roughness elements. Exp. Fluids 51 (5), 13431352.Google Scholar