A wall-wake model for the turbulence structure of boundary layers. Part 1. Extension of the attached eddy hypothesis

Author:

Perry A. E.,Marušić Ivan

Abstract

The attached eddy hypothesis developed for zero pressure gradient boundary layers and for pipe flow is extended here to boundary layers with arbitrary streamwise pressure gradients, both favourable and adverse. It is found that in order to obtain the correct quantitative results for all components of the Reynolds stresses, two basic types of eddy structure geometries are required. The first type, called type-A, is interpreted to give a ‘wall structure’ and the second, referred to as type-B, gives a ‘wake structure’. This is in analogy with the conventional mean velocity formulation of Coles where the velocity is decomposed into a law of the wall and a law of the wake.If the above mean velocity formulation is accepted, then in principle, once the eddy geometries are fixed for the two eddy types, all Reynolds stresses and associated spectra contributed from the attached eddies can be computed without any further empirical constants. This is done by using the momentum equation and certain convolution integrals developed here based on the attached eddy hypothesis. The theory is developed using data from equilibrium and quasi-equilibrium flows. In Part 2 the authors’ non-equilibrium data are used.

Publisher

Cambridge University Press (CUP)

Subject

Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics

Reference23 articles.

1. Rotta, J. C. 1962 Turbulent boundary layers in incompressible flow.Prog. Aero. Sci. 2,1–219.

2. Perry, A. E. & Chong, M. S. 1982 On the mechanism of wall turbulence.J. Fluid Mech. 119,173–217.

3. Perry, A. E. & Li, J. D. 1990 Experimental support for the attached eddy hypothesis in zeropressure-gradient turbulent boundary layers.J. Fluid Mech. 218,405–438.

4. Winckelmans, G. S. & Leonard, A. 1993 Contributions to vortex particle methods for the computation of three-dimensional incompressible unsteady flows.J. Comput. Phys. 109,247–273.

5. Coles, D. E. 1956 The law of the wake in the turbulent boundary layer.J. Fluid Mech. 1,191–226.

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