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Contributions of the wall boundary layer to the formation of the counter-rotating vortex pair in transverse jets

Published online by Cambridge University Press:  08 April 2011

FABRICE SCHLEGEL*
Affiliation:
Department of Mechanical Engineering, Massachusetts Institute of Technology, Cambridge, MA 02139, USA
DAEHYUN WEE
Affiliation:
Department of Environmental Science and Engineering, Ewha Womans University, Seoul 120-750, Republic of Korea
YOUSSEF M. MARZOUK
Affiliation:
Department of Aeronautics and Astronautics, Massachusetts Institute of Technology, Cambridge, MA 02139, USA
AHMED F. GHONIEM
Affiliation:
Department of Mechanical Engineering, Massachusetts Institute of Technology, Cambridge, MA 02139, USA
*
Email address for correspondence: [email protected]

Abstract

Using high-resolution 3-D vortex simulations, this study seeks a mechanistic understanding of vorticity dynamics in transverse jets at a finite Reynolds number. A full no-slip boundary condition, rigorously formulated in terms of vorticity generation along the channel wall, captures unsteady interactions between the wall boundary layer and the jet – in particular, the separation of the wall boundary layer and its transport into the interior. For comparison, we also implement a reduced boundary condition that suppresses the separation of the wall boundary layer away from the jet nozzle. By contrasting results obtained with these two boundary conditions, we characterize near-field vortical structures formed as the wall boundary layer separates on the backside of the jet. Using various Eulerian and Lagrangian diagnostics, it is demonstrated that several near-wall vortical structures are formed as the wall boundary layer separates. The counter-rotating vortex pair, manifested by the presence of vortices aligned with the jet trajectory, is initiated closer to the jet exit. Moreover tornado-like wall-normal vortices originate from the separation of spanwise vorticity in the wall boundary layer at the side of the jet and from the entrainment of streamwise wall vortices in the recirculation zone on the lee side. These tornado-like vortices are absent in the case where separation is suppressed. Tornado-like vortices merge with counter-rotating vorticity originating in the jet shear layer, significantly increasing wall-normal circulation and causing deeper jet penetration into the crossflow stream.

Type
Papers
Copyright
Copyright © Cambridge University Press 2011

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References

REFERENCES

Broadwell, J. E. & Breidenthal, R. E. 1984 Structure and mixing of a transverse jet in incompressible-flow. J. Fluid Mech. 148, 405412.CrossRefGoogle Scholar
Coelho, S. L. V. & Hunt, J. C. R. 1989 The dynamics of the near-field of strong jets in crossflows. J. Fluid Mech. 200, 95120.CrossRefGoogle Scholar
Cortelezzi, L. & Karagozian, A. R. 2001 On the formation of the counter-rotating vortex pair in transverse jets. J. Fluid Mech. 446, 347373.CrossRefGoogle Scholar
Cottet, G.-H. & Koumoutsakos, P. D. 2000 Vortex Methods: Theory and Practice. Cambridge University Press.CrossRefGoogle Scholar
Fric, T. F. & Roshko, A. 1994 Vortical structure in the wake of a transverse jet. J. Fluid Mech. 279, 147.CrossRefGoogle Scholar
Kamotani, Y. & Greber, I. 1972 Experiments on a turbulent jet in a cross flow. AIAA J. 10, 14251429.CrossRefGoogle Scholar
Keffer, J. F. & Baines, W. D. 1962 The round turbulent jet in a cross-wind. J. Fluid Mech. 15, 481496.CrossRefGoogle Scholar
Kelso, R. M., Lim, T. T. & Perry, A. E. 1996 An experimental study of round jets in cross-flow. J. Fluid Mech. 306, 111144.CrossRefGoogle Scholar
Leonard, A. 1985 Computing three-dimensional incompressible flows with vortex elements. Annu. Rev. Fluid Mech. 17, 523559.CrossRefGoogle Scholar
Lim, T. T., New, T. H. & Luo, S. C. 2001 On the development of large-scale structures of a jet normal to a cross flow. Phys. Fluids 13 (3), 770775.CrossRefGoogle Scholar
Lindsay, K. & Krasny, R. 2001 A particle method and adaptive treecode for vortex sheet motion in three-dimensional flow. J. Comput. Phys. 172 (2), 879907.CrossRefGoogle Scholar
Majda, A. & Bertozzi, A. L. 2002 Vorticity and Incompressible Flow. Cambridge University Press.Google Scholar
Margason, R. J. 1968 The path of a jet directed at large angles to a subsonic free stream. NASA Technical Note D-4919.Google Scholar
Marzouk, Y. M. & Ghoniem, A. F. 2005 k-means clustering for optimal partitioning and dynamic load balancing of parallel hierarchical N-body simulations. J. Comput. Phys. 207, 493528.CrossRefGoogle Scholar
Marzouk, Y. M. & Ghoniem, A. F. 2007 Vorticity structure and evolution in a transverse jet. J. Fluid Mech. 575, 267305.CrossRefGoogle Scholar
Moore, D. W. 1972 Finite amplitude waves on aircraft trailing vortices. Aeronaut. Q. 23, 307314.CrossRefGoogle Scholar
Muppidi, S. & Mahesh, K. 2005 Study of trajectories of jets in crossflow using direct numerical simulations. J. Fluid Mech. 530, 81100.CrossRefGoogle Scholar
Rosenhead, L. 1931 The formation of vortices from a surface of discontinuity. Proc. R. Soc. A 134, 170192.Google Scholar
Schlegel, F., Wee, D. & Ghoniem, A. F. 2008 A fast 3d particle method for the simulation of buoyant flow. J. Comput. Phys. 227 (21), 90639090.CrossRefGoogle Scholar
Smith, S. H. & Mungal, M. G. 1998 Mixing, structure, and scaling of the jet in crossflow. J. Fluid Mech. 357, 83122.CrossRefGoogle Scholar
Wee, D. & Ghoniem, A. F. 2006 Modified interpolation kernels for diffusion and remeshing in vortex methods. J. Comput. Phys. 213, 239263.CrossRefGoogle Scholar
Wu, J. M., Vakili, A. D. & Yu, F. M. 1988 Investigation of the interacting flow of nonsymmetric jets in crossflow. AIAA J. 26, 940947.CrossRefGoogle Scholar
Yuan, L. L., Street, R. L. & Ferziger, J. H. 1999 Large-eddy simulations of a round jet in crossflow. J. Fluid Mech. 379, 71104.CrossRefGoogle Scholar