Boussinesq's Turbulent Viscosity Hypothesis
For simple turbulent shear flows, Boussinesq in 1877 proposed the idea of
eddy viscosity (also called turbulent viscosity)
A simple turbulent shear flow is one in which one single shear-rate component dominates; examples include a two-dimensional turbulent mixing layer, a two-dimensional or axisymmetric jet, an axisymmetric wake, and a two-dimensional boundary layer over a wall.
In these cases the Reynolds shear stress $-\rho\,\overline{u_1 u_2}$ plays the main role in the mean flow.
By analogy with Newton's law of viscosity for a Newtonian fluid, Boussinesq proposed the turbulent viscosity hypothesis
$$
-\rho\,\overline{u_1 u_2} \;=\; \mu_t\,\frac{\partial U_1}{\partial x_2}
$$
where $\mu_t$ is the turbulent viscosity coefficient or eddy viscosity coefficient
For more complex turbulent flows, by analogy with the Newtonian law one further assumes that the Reynolds-stress tensor is related to the mean rate-of-strain tensor by
$$
\overline{u_i u_j}
=\frac{2}{3}\,k\,\delta_{ij}
-\nu_t\!\left(\frac{\partial U_i}{\partial x_j}
+\frac{\partial U_j}{\partial x_i}\right)
$$
where $k$ is the turbulent kinetic energy per unit mass, $\delta_{ij}$ is the Kronecker delta, and $\nu_t=\mu_t/\rho$ is the kinematic eddy viscosity
\(\boxed{\overline{u_i u_j}
=\frac{2}{3}\,k\,\delta_{ij}
-\nu_t\!\left(\frac{\partial U_i}{\partial x_j}
+\frac{\partial U_j}{\partial x_i}\right)}\) is the Boussinesq's turbulent viscosity hypothesis.
For incompressible flow, let $i=j$ yields
$
\overline{u_i u_i}=2k
$,
which is consistent with the definition of $k$
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