Reynolds-averaged Navier–Stokes equations

Reynolds-averaged Navier–Stokes equations

The Reynolds-averaged Navier–Stokes (RANS) equations are time-averaged [The true time average ( ar{X} ) of a variable ( x ) is defined by: ar{X} = lim_{T o infty}frac{1}{T}int_{t_0}^{t_0+T} x, dt. For this to be a well-defined term, the limit ( ar{X} ) must be independent of the initial condition at t_0. In the case of a chaotic dynamical system, which the equations under turbulent conditions are thought to be, this means that the system can have only one strange attractor, a result that has yet to be proved for the Navier-Stokes equations. However, assuming the limit exists (which it does for any bounded system, which fluid velocities certainly are), there exists some T such that integration from t_0 to T is arbitrarily close to the average. This means that given transient data over a sufficiently large time, the average can be numerically computed within some small error. However, there is no analytical way to obtain an upper bound on T.] equations of motion for fluid flow. They are primarily used while dealing with turbulent flows. These equations can be used with approximations based on knowledge of the properties of flow turbulence to give approximate averaged solutions to the Navier–Stokes equations.For a stationary, incompressible flow of Newtonian fluid, these equations can be written as :

ho frac{partial ar{u}_j ar{u}_i }{partial x_j}= ho ar{f}_i+ frac{partial}{partial x_j} left [ - ar{p}delta_{ij} + mu left( frac{partial ar{u}_i}{partial x_j} + frac{partial ar{u}_j}{partial x_i} ight)- ho overline{u_i^prime u_j^prime} ight ] .

The left hand side of this equation represents the change in mean momentum of fluid element due to the unsteadiness in the mean flow and the convection by the mean flow. This change is balanced by the mean body force, the isotropic stress due to the mean pressure field, the viscous stresses, and apparent stress left( - ho overline{u_i^prime u_j^prime} ight) due to the fluctuating velocity field, generally referred to as Reynolds stresses.

Derivation of RANS equations

The basic tool required for the derivation of the RANS equations from the instantaneous Navier–Stokes equations is the "Reynolds decomposition". Reynolds decomposition refers to separation of the flow variable (like velocity u ) into the mean (time-averaged) component (ar{u}) and the fluctuating component (u^prime). [ By definition, the mean of the fluctuating quantity is zero( ar{u^prime} = 0). ] Thus,

: u(mathbf{x},t) = ar{u}(mathbf{x}) + u^prime(mathbf{x},t) , [Some authors prefer using U instead of ar{u} for the mean term (since an overbar is used to represent a vector). Also it is common practice to represent the fluctuating term u^prime by u , even though u refers to the instantaneous value. This is possible because the two terms do not appear simultaneously in the same equation. To avoid confusion we will use u, ar{u}, mbox{ and }u^prime to represent the instantaneous, mean and fluctuating term. ] where, mathbf{x} = (x,y,z) is the position vector.

The following rules will be useful while deriving the RANS. If f and g are two flow variables (like density ( ho ), velocity ( u ), pressure ( p ), etc.) and s is one of the independent variables ( x,y,z, mbox{ or } t ) then,

: overline{overline{f = ar{f} : overline{f+g} = ar{f} + ar{g} : overline{overline{f}g} = ar{f}ar{g} : overline{fg} e ar{f}ar{g} : overline{frac{partial f}{partial s = frac{partial ar{f{partial s}

Now the Navier–Stokes equations of motion [The equations are expressed in tensor notation, which greatly simplifies the maths.] for an incompressible Newtonian fluid are:

: frac{partial u_i}{partial x_i} = 0 : frac{partial u_i}{partial t} + u_j frac{partial u_i}{partial x_j}= f_i - frac{1}{ ho} frac{partial p}{partial x_i}+ u frac{partial^2 u_i}{partial x_j partial x_j}

Substituting, u_i = ar{u_i} + u_i^prime, p = ar{p} + p^prime , etc. [: frac{partial left( ar{u_i} + u_i^prime ight)}{partial x_i} = 0 : frac{partial left( ar{u_i} + u_i^prime ight)}{partial t}+ left( ar{u_j} + u_j^prime ight) frac{partial left( ar{u_i} + u_i^prime ight)}{partial x_j}= left( ar{f_i} + f_i^prime ight)- frac{1}{ ho} frac{partial left(ar{p} + p^prime ight)}{partial x_i} + u frac{partial^2 left( ar{u_i} + u_i^prime ight)}{partial x_j partial x_j}

Time averaging these equations yields,: overline{frac{partial left( ar{u_i} + u_i^prime ight)}{partial x_i = 0 : overline{frac{partial left( ar{u_i} + u_i^prime ight)}{partial t+ overline{left( ar{u_j} + u_j^prime ight) frac{partial left( ar{u_i} + u_i^prime ight)}{partial x_j= overline{left( ar{f_i} + f_i^prime ight)}- frac{1}{ ho} overline{frac{partial left(ar{p} + p^prime ight)}{partial x_i+ u overline{frac{partial^2 left( ar{u_i} + u_i^prime ight)}{partial x_j partial x_j

Note that the nonlinear terms (like overline{u_i u_i} ) can be simplified to,

overline{u_i u_i} = overline{left( ar{u_i} + u_i^prime ight)left( ar{u_i} + u_i^prime ight) }= overline{ar{u_i}ar{u_i} + ar{u_i}u_i^prime + u_i^primear{u_i} + u_i^prime u_i^prime}= ar{u_i}ar{u_i} + overline{u_i^prime u_i^prime} ] and taking a time-average of these equations yields,

: frac{partial ar{u_i{partial x_i} = 0: frac{partial ar{u_i{partial t} + ar{u_j}frac{partial ar{u_i} }{partial x_j}+ overline{u_j^prime frac{partial u_i^prime }{partial x_j= ar{f_i}- frac{1}{ ho}frac{partial ar{p{partial x_i}+ u frac{partial^2 ar{u_i{partial x_j partial x_j}

The momentum equation can also be written as, [This follows from the mass conservation equation which gives,: frac{partial u_i}{partial x_i} = frac{partial ar{u_i{partial x_i} + frac{partial u_i^prime}{partial x_i} = 0] : frac{partial ar{u_i{partial t} + frac{partial ar{u_j} ar{u_i} }{partial x_j}= ar{f_i}- frac{1}{ ho}frac{partial ar{p{partial x_i}+ u frac{partial^2 ar{u_i{partial x_j partial x_j}- frac{partial overline{u_i^prime u_j^prime {partial x_j}On further manipulations this yields,: ho frac{partial ar{u_i{partial t} + ho frac{partial ar{u_j} ar{u_i} }{partial x_j}= ho ar{f_i}+ frac{partial}{partial x_j} left [ - ar{p}delta_{ij} + 2mu ar{S_{ij- ho overline{u_i^prime u_j^prime} ight ]

where,ar{S_{ij = frac{1}{2}left( frac{partial ar{u_i{partial x_j} + frac{partial ar{u_j{partial x_i} ight)is the mean rate of strain tensor.

Finally, since integration in time removes the time dependence of the resultant terms, the time derivative must be eliminated, leaving:: ho frac{partial ar{u_j} ar{u_i} }{partial x_j}= ho ar{f_i}+ frac{partial}{partial x_j} left [ - ar{p}delta_{ij} + 2mu ar{S_{ij- ho overline{u_i^prime u_j^prime} ight ]


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