230 12 Integral Formulae and Distribution Functions
withx=exνrνandy=e
y
νrν, whereexandeyare unit vectors parallel to thex-axis
andy-axis, respectively. The unit vector parallel to thez-axis isez. The constant shear
rate is
γ=
∂vx
∂y
. (12.126)
The vorticity and the shear rate tensor, cf. are
ωλ=−
1
2
γezλ,γμν=γ eyνexμ =
1
2
γ(eyνexμ+eyμexν). (12.127)
Here, the first order expression (12.121) implies
δg(^1 )=−τγxyr−^1 g′eq,
and one has
gμν=−τγrg′eqeyνexμ,
in this approximation. The more general ansatz
gμν=g+eyνexμ+g−
1
2
(exνexμ−eyνeyμ)+g 0 ezνezμ (12.128)
contains all terms which obey the plane Couette symmetry, viz. which are invariant
when bothexandeyare replaced by−exand−ey. The remaining two terms of the 5
components of the irreducible second rank tensor which, however, do not have this
symmetry, are proportional toezνexμ andezνeyμ.
The quantitiesg+,g−andg 0 are functions ofr. In first order in the shear rateγ,
one hasg+=−τγr−^1 g′eqandg−=g 0 =0. In second order,g−=γτg+,g 0 = 0
is found. The calculation is deferred to the next exercise.
12.4 Exercise: Pair Correlation Distorted by a Couette Flow
Compute the functionsg+,g−andg 0 in first and second order in the shear rateγ,in
steady state, from the plane Couette version of the kinetic equation (12.120)
γy
∂
∂x
δg+τ−^1 δg=−γy
∂
∂x
geq.
Hint:usey^2 =(x^2 +y^2 )/ 2 −(x^2 −y^2 )/2 andx^2 +y^2 =r^2 −z^2 = 2 r^2 / 3 −(z^2 −r^2 / 3 ),
furthermore decomposex^2 y^2 =exμexνeyλeyκrμrνrλrκinto its parts associated with
tensors of ranks= 0 , 2 ,4 with the help of (9.6). Compareg−withg+.