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Oscillations, Waves, and Interactions - GWDG

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Sound absorption, sound amplification, <strong>and</strong> flow control in ducts 89<br />

Herein ɛµ comprises the transport of energy due to viscosity, i. e., diffusion <strong>and</strong> dissipation,<br />

which will be disregarded, to begin with. Thus the power extracted from the<br />

mean flow (left-h<strong>and</strong> side of Eq. (5)) is fed into the streamwise flux of kinetic energy<br />

<strong>and</strong> into the wall-normal energy transport due to the pressure-velocity correlation<br />

(first <strong>and</strong> second term on the right-h<strong>and</strong> side, respectively). While the wall-normal<br />

energy transport balances the dissipation of energy in the walls <strong>and</strong> therefore is irreversible,<br />

the kinetic energy contained in oscillation of the flow can be returned to<br />

the mean flow if the Reynolds shear stress becomes negative. Under this condition<br />

the first term on the right-h<strong>and</strong> side is negative as well, meaning that the amplitude<br />

of the oscillation decreases in the mean-flow direction, <strong>and</strong> we will see from Eq. (7)<br />

that the static pressure may increase under the same condition.<br />

3.1.3 Static pressure gradient<br />

The supply or the recovery of mean flow energy in a homogeneous channel cannot<br />

change the kinetic energy of the mean flow when the velocity profile is assumed to<br />

remain constant along the axial coordinate x. Hence the exchange of energy must<br />

be balanced by the work done by the pressure gradient on the flow. For the sake<br />

of simplicity, the following formulae are restricted to the 2D channel (half-width R)<br />

<strong>and</strong> to the channel with circular cross-section (radius R). The wall shear stress τ w<br />

is constant over the circumference ∂(S) of the channel in both these cases. So the<br />

balance between the forces due to the pressure gradient, due to the wall friction, <strong>and</strong><br />

due to the acceleration of the fluid yields<br />

− dp<br />

dx = τ ∂(S) d<br />

w +<br />

S dx<br />

�<br />

S<br />

2 dS<br />

ρU . (6)<br />

S<br />

The axial pressure gradient dp/dx is assumed to be constant over the cross-section<br />

which is a good approximation except for extreme axial alteration of the mean velocity<br />

profile U(r, x). We are particularly interested in the first term on the righth<strong>and</strong><br />

side of Eq. (6) which is due to the wall shear stress <strong>and</strong> which will be denoted<br />

by dp τ /dx. After some analysis the work done by dp τ /dx on the flow, namely<br />

�<br />

S (dp τ /dx)U dS, can be equated with<br />

�<br />

−<br />

S<br />

dp τ<br />

dx UdS = τ wU∂(S)<br />

τ µ≪τ ′′<br />

=<br />

�<br />

0<br />

R<br />

�<br />

τ dU<br />

dy<br />

� S<br />

R dy<br />

� �� �<br />

2D channel<br />

τ µ≪τ ′′<br />

=<br />

�<br />

0<br />

R<br />

�<br />

τ<br />

�<br />

− dU<br />

dr<br />

��<br />

2πrdr<br />

� �� �<br />

circular duct<br />

(7)<br />

wherein<br />

τ(r) = τ ′′ r<br />

(r) + τ µ(r) = τ w<br />

(8)<br />

R<br />

has been used which applies to the circular duct as well as to the 2D channel with<br />

r = R − y. So, according to the middle part of Eq. (8), the right-h<strong>and</strong> side of Eq. (7)<br />

comprises the power that is fed into the oscillation of the flow according to Eq. (5)<br />

<strong>and</strong> the power that is dissipated by the mean viscous shear stress τ µ. Furthermore<br />

it turns out that the wall shear stress is a measure of the considered energy transfer.

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