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Direct numerical simulation of a decelerated wall-bounded turbulent shear flow

Published online by Cambridge University Press:  11 November 2003

G. N. COLEMAN
Affiliation:
School of Engineering Sciences, University of Southampton, Highfield Campus, Southampton, SO17 1BJ, UK
J. KIM
Affiliation:
Mechanical and Aerospace Engineering, University of California, Los Angeles, CA 90095, USA
P. R. SPALART
Affiliation:
Boeing Commercial Airplanes, Seattle, WA 98124, USA

Abstract

A fully developed turbulent channel flow is subjected to a mean strain that approximates that in a spatially developing adverse-pressure-gradient (APG) boundary layer. This is done by applying uniform irrotational temporal deformations to the flow domain of a conventional direct numerical simulation channel code. The velocity difference between the inner and outer layer is also controlled by accelerating the walls in the streamwise plane, in order to duplicate the defining features of both the inner and outer regions of an APG boundary layer. Eventually, the flow reverses at the wall. We address basic physics and modelling issues, and create a database that makes detailed testing of turbulence models easy. As in the corresponding spatial layers, distinct inner- and outer-layer dynamics are observed: a decrease in turbulence intensity near the wall is accompanied by increased energy in the outer layer. The ‘extra strain’ effect associated with the diverging outer-layer streamlines is documented, particularly in the Reynolds-stress budgets.

Type
Papers
Copyright
© 2003 Cambridge University Press

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