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Oscillations, Waves, and Interactions - GWDG

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88 D. Ronneberger et al.<br />

e. g. temporal, is taken of the equation, as was applied in the decomposition of the<br />

field quantities. As a result the mean transport of momentum which is described by<br />

the tensor ρuu t is composed of two parts: ρuu t = ρ u ′ u ′ t + ρ u u t wherein the<br />

fluctuation of the density is disregarded. So the fluctuation of the velocity contributes<br />

to the mean transport of momentum by the covariance of the velocity components.<br />

The term −ρ u ′ u ′ t is also known as Reynolds stress tensor because it contributes to<br />

the balance of forces between the volume elements in the same way as the pressure<br />

<strong>and</strong> the viscous friction. Particularly the Reynolds shear stress τ ′′ := −ρu ′ v ′ which<br />

exceeds the viscous shear stress τ µ := µ ∂ u/∂y by orders of magnitude in turbulent<br />

flow, plays the dominant role in the development of the mean flow profile.<br />

On the other h<strong>and</strong>, the mean velocity profile is crucial to the development of the<br />

Reynolds tensor. To underst<strong>and</strong> this we consider the hypothetical case that the<br />

fluctuating part of the flow consists of a single mode of a small-amplitude oscillation<br />

so that the Navier Stokes equation can be linearized. Additionally we confine our<br />

consideration to the simple incompressible flow u = [U(y), 0, 0] t in a 2D channel<br />

where we can use the wave ansatz<br />

{u ′ , v ′ , p ′ }(x, y, t) = {û, ˆv, ˆp}(y) · exp[i(αx − ωt)] (3)<br />

(with angular frequency ω, wavenumber α, axial <strong>and</strong> wall-normal space coordinates<br />

x <strong>and</strong> y). Then the Orr-Sommerfeld equation is obtained for the amplitude ˆv(y) of<br />

the wall-normal component of the flow velocity. This is a fourth-order differential<br />

equation which reduces to the second order Rayleigh equation if the effects of viscosity<br />

are disregarded:<br />

d2ˆv =<br />

dy2 �<br />

α 2 + d2 U/dy 2<br />

U − ω/α<br />

�<br />

·ˆv ; û = i<br />

dˆv<br />

α dy<br />

�<br />

i<br />

; ˆp = ρ<br />

α<br />

dU<br />

�<br />

ˆv − i(ω − αU)ρû<br />

dy<br />

<strong>and</strong> for the sake of completeness the Rayleigh equation has been supplemented by<br />

relations for û <strong>and</strong> ˆp. Together with the boundary conditions at the walls an eigenvalue<br />

problem is established which generally has a number of solutions ω = Ω n(α).<br />

Each of these solutions is the dispersion relation of a mode which may contribute to<br />

the fluctuating part of the flow. It is obvious from the Rayleigh equation (4) that<br />

the dispersion relations <strong>and</strong> consequently (û, ˆv)n as well as the Reynolds shear stress<br />

τ ′′ n = −ρ 1<br />

2 ℜ{û · ˆv∗ }n depend on the mean flow profile, in particular on d 2 U/dy 2 .<br />

Furthermore it should be noted that τ ′′ n crucially depends on the phase difference<br />

between û <strong>and</strong> ˆv <strong>and</strong> hence can appear also as a negative-friction force.<br />

3.1.2 Exchange of energy between mean flow <strong>and</strong> flow oscillation<br />

The Reynolds shear stress is essential for the exchange of energy between the mean<br />

flow <strong>and</strong> the flow oscillation. The rate at which energy per volume is transferred<br />

from the mean to the oscillating part of the flow is given by the product of shear<br />

stress <strong>and</strong> shear rate τ ′′ · dU/dy (angular momentum × angular velocity). From the<br />

incompressible Navier Stokes equations, one obtains<br />

τ ′′ · dU<br />

dy = −ρu′ v ′ · dU<br />

dy<br />

(4)<br />

d ρ<br />

= U<br />

dx 2 u′2 + v ′2 + d<br />

dy p′ v ′ + ɛµ . (5)

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