A theory is proposed in this paper to describe the behaviour of a class of turbulent shear flows as the Reynolds number approaches infinity. A detailed analysis is given for simple representative members of this class, such as fully developed channel and pipe flows and two-dimensional turbulent boundary layers. The theory considers an underdetermined system of equations and depends critically on the idea that these flows consist of two rather different types of regions. The method of matched asymptotic expansions is employed together with asymptotic hypotheses describing the order of various terms in the equations of mean motion and turbulent kinetic energy. As these hypotheses are not closure hypotheses, they do not impose any functional r...
In this chapter, a steady laminar axisymmetrical flow in a straight constricted pipe is considered (...
A theoretical investigation is made of the mixing layer between two streams. The work is divided int...
The interaction due to an unseparated supersonic turbulent boundary layer at a two-dimensional compr...
Understanding of the structure of turbulent flows at extreme Reynolds numbers (Re) is relevant becau...
Effects of moderately large Reynolds numbers R are studied by considering higher order terms in the ...
The present approach to matched asymptotic expansions in turbulent flow is based on a systematic app...
Communication to : Proceedings IUTAM, Bochum (DE), June 28-30, 1995SIGLEAvailable at INIST (FR), Doc...
We study the heat transfer in the layer plane boundary of an incompressible fluid when the Reynolds ...
The turbulent boundary layer is one of the most fundamental and important applications of fluid mech...
A new turbulence approach based on Lie-group analysis is presented. It unifies a large set of self-s...
Equilibrium turbulent boundary-layer is analyzed within the framework of the asymptotic theory for l...
Abstract. This article surveys the asymptotic theory of high Reynolds num-ber steady flows in two di...
We interpret experimental results on the structure of an open channel flow with a strong transverse ...
A new turbulence theory based on Lie-group analysis is presented. This theory unifies a large set of...
The streamwise velocity component in turbulent pipe flow is assessed to determine whether it exhibit...
In this chapter, a steady laminar axisymmetrical flow in a straight constricted pipe is considered (...
A theoretical investigation is made of the mixing layer between two streams. The work is divided int...
The interaction due to an unseparated supersonic turbulent boundary layer at a two-dimensional compr...
Understanding of the structure of turbulent flows at extreme Reynolds numbers (Re) is relevant becau...
Effects of moderately large Reynolds numbers R are studied by considering higher order terms in the ...
The present approach to matched asymptotic expansions in turbulent flow is based on a systematic app...
Communication to : Proceedings IUTAM, Bochum (DE), June 28-30, 1995SIGLEAvailable at INIST (FR), Doc...
We study the heat transfer in the layer plane boundary of an incompressible fluid when the Reynolds ...
The turbulent boundary layer is one of the most fundamental and important applications of fluid mech...
A new turbulence approach based on Lie-group analysis is presented. It unifies a large set of self-s...
Equilibrium turbulent boundary-layer is analyzed within the framework of the asymptotic theory for l...
Abstract. This article surveys the asymptotic theory of high Reynolds num-ber steady flows in two di...
We interpret experimental results on the structure of an open channel flow with a strong transverse ...
A new turbulence theory based on Lie-group analysis is presented. This theory unifies a large set of...
The streamwise velocity component in turbulent pipe flow is assessed to determine whether it exhibit...
In this chapter, a steady laminar axisymmetrical flow in a straight constricted pipe is considered (...
A theoretical investigation is made of the mixing layer between two streams. The work is divided int...
The interaction due to an unseparated supersonic turbulent boundary layer at a two-dimensional compr...