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Journal ArticleDOI

Application of a new effective viscosity model to turbulent plane Couette flow

Seck Hong Chue, +1 more
- 01 Nov 1970 - 
- Vol. 8, Iss: 11, pp 2076-2078
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TLDR
AjC as discussed by the authors describes the constants occurring in semi-logarithmic laws for turbulent layers of the Couette flow system, including the skin-friction coefficient and the Reynolds number.
Abstract
AjC — constants occurring in semi-logarithmic laws for turbulent layers Cf = skin-friction coefficient, rwl\pu^ h = half width of channel Re = Reynolds number based on half width, huc/v S = dimensionless centerline velocity gradient, (h/uc)du/dy)c u = velocity in streamwise direction u* = friction velocity, (r^/p) u = dimensionless velocity, ufu* U = relative velocity between planes of the Couette flow system y = coordinate normal to wall y + = dimensionless wall distance, yu*/v z = dimensionless wall distance, y/h 7 = dimensionless ratio of effective to kinematic viscosity p = fluid density T = shear stress v = kinematic viscosity

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Journal ArticleDOI

Asymptotic analysis of plane turbulent Couette-Poiseuille flows

TL;DR: In this article, a matched asymptotic expansion was used to describe turbulent Couette-Poiseuille flow (plane duct flow with a pressure gradient and a moving wall) and a special modification of conventional eddy-diffusivity closure accounts for the experimentally observed non-coincidence of the locations of zero shear stress and maximum velocity.
Journal ArticleDOI

Modeling plane turbulent Couette flow

TL;DR: In this paper, a second-moment closure study of turbulent Couette flow is presented, where the authors use a wall-proximity function in the wall-reflection part of the pressure-strain model.
Proceedings ArticleDOI

Modelling plane turbulent Couette flow

Journal ArticleDOI

General mean velocity distribution law for smooth-wall plane couette flow

TL;DR: The plane couette flow between two parallel smooth walls is one of the classic wall-bounded shear flows as discussed by the authors, and its analysis is limited to the linear law for laminar flow.
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