Finite volume method

The finite volume method is a method for representing and evaluating partial differential equations as algebraic equations. Similar to the finite difference method, values are calculated at discrete places on a meshed geometry. "Finite volume" refers to the small volume surrounding each node point on a mesh. In the finite volume method, volume integrals in a partial differential equation that contain a divergence term are converted to surface integrals, using the divergence theorem. These terms are then evaluated as fluxes at the surfaces of each finite volume. Because the flux entering a given volume is identical to that leaving the adjacent volume, these methods are conservative. Another advantage of the finite volume method is that it is easily formulated to allow for unstructured meshes. The method is used in many computational fluid dynamics packages.

1D example

Consider a simple 1D advection problem defined by the following partial differential equation

:quad (1) qquad qquad frac{partial ho}{partial t}+frac{partial f}{partial x}=0,quad tge0.

Here, ho= ho left( x,t ight) represents the state variable and f=f left( ho left( x,t ight) ight) represents the flux or flow of ho . Conventionally, positive f represents flow to the right whilst negative f represents flow to the left. If we assume that equation (1) represents a flowing medium of constant area, we can sub-divide the spatial domain, x , into "finite volumes" or "cells" with cell centres indexed as i . For a particular cell, i , we can define the "volume average" value of { ho }_i left( t ight) = ho left( x, t ight) at time {t = t_1 } and { x in left [ x_{i-frac{1}{2 , x_{i+frac{1}{2 ight] } , as

:quad (2) qquad qquad ar{ ho}_i left( t_1 ight) = frac{1}{ x_{i+frac{1}{2 - x_{i-frac{1}{2} int_{x_{i-frac{1}{2}^{x_{i+frac{1}{2} ho left(x,t_1 ight), dx ,

and at time {t = t_2} as,

:quad (3) qquad qquad ar{ ho}_i left( t_2 ight) = frac{1}{x_{i+frac{1}{2 - x_{i-frac{1}{2} int_{x_{i-frac{1}{2}^{x_{i+frac{1}{2} ho left(x,t_2 ight), dx ,

where x_{i-frac{1}{2 and x_{i+frac{1}{2 represent locations of the upstream and downstream faces or edges respectively of the i^{th} cell.

Integrating equation (1) in time, we have:

:quad (4) qquad qquad ho left( x, t_2 ight) = ho left( x, t_1 ight) + int_{t_1}^{t_2} f_x left( ho left( x,t ight) ight), dt.

To obtain the volume average of holeft(x,t ight) at time t=t_{2} , we integrate holeft(x,t_2 ight) over the cell volume, v_i and divide the result by v_i , i.e.

: quad (5) qquad qquad ar{ ho}_{i}left( t_{2} ight) =frac{1}{v_i}int_{v_i}left{ holeft( x,t_{1} ight) +int_{t_{1^{t_2}f_{x}left( ho left( x,t ight) ight) dt ight} dv.

We assume that f is well behaved and that we can reverse the order of integration. Also, recall that flow is normal to the unit area of the cell. Now, since in one dimension f_x riangleq abla f , we can apply the divergence theorem and substitute for the volume integral of the divergence with the values of f(x) at the cell edges x_{i-frac{1}{2 and x_{i+frac{1}{2 of the finite volume as follows:

:quad (6) qquad qquad ar{ ho}_i left( t_2 ight) = frac{1}{Delta x_{i left [ int_{x_{i-frac{1}{2}^{x_{i+frac{1}{2} ho left(x,t_1 ight), dx + int_{t_1}^{t_2} f_{i + frac{1}{2 dt- int_{t_1}^{t_2} f_{i - frac{1}{2 dt ight] .

where Delta x_i = x_{i+frac{1}{2-x_{i-frac{1}{2 and f_{i pm frac{1}{2 =f left( ho left( x_{i pm frac{1}{2, t ight) ight) .

We can therefore derive a "semi-discrete" numerical scheme for the above problem with cell centres indexed as i , and with cell edge fluxes indexed as ipmfrac{1}{2} , by differentiating (6) with respect to time to obtain:

:quad (7) qquad qquad frac{d ar{ ho}_i}{d t} + frac{1}{Delta x_i} left [ f_{i + frac{1}{2 - f_{i - frac{1}{2 ight] =0 ,

where values for the edge fluxes, f_{i pm frac{1}{2 , can be reconstructed by interpolation or extrapolation of the cell averages. It should be noted that equation (7) is "exact" for the volume averages; i.e., no approximations have been made during its derivation.

General hyperbolic problem

We can also consider a general hyperbolic problem, represented by the following PDE,

: quad (8) qquad qquad partial {mathbf u over {partial t + abla cdot {mathbf f}left( {mathbf u } ight) = {mathbf 0} .

Here, {mathbf u} represents a vector of states and mathbf f represents the corresponding flux vector. Again we can sub-divide the spatial domain into finite volumes or cells. For a particular cell, i , we take the volume integral over the total volume of the cell, v _{i} , which gives,

: quad (9) qquad qquad int _{v_{i partial {mathbf u over {partial t, dv + int _{v_{i abla cdot {mathbf f}left( {mathbf u } ight), dv = {mathbf 0} .

On integrating the first term to get the "volume average" and applying the "divergence theorem" to the second, this yields

:quad (10) qquad qquad v_{i} d {mathbf {ar u} }_{i} } over {dt + oint _{S_{i} } {mathbf f} left( {mathbf u } ight) dS = {mathbf 0},

where S_{i} represents the total surface area of the cell. So, finally, we are able to present the general result equivalent to (7), i.e.

: quad (11) qquad qquad d {mathbf {ar u} }_{i} } over {dt + 1} over {v_{i } oint _{S_{i} } {mathbf f} left( {mathbf u } ight) dS = {mathbf 0} .

Again, values for the edge fluxes can be reconstructed by interpolation or extrapolation of the cell averages. The actual numerical scheme will depend upon problem geometry and mesh construction. MUSCL reconstruction is often used in high resolution schemes where shocks or discontinuities are present in the solution.

Finite volume schemes are conservative as cell averages change through the edge fluxes. In other words, "one cell's loss is another cell's gain"!

ee also

*Flux limiter
*Godunov's theorem
*High-resolution scheme
*MUSCL scheme
*Sergei K. Godunov
*Total variation diminishing
*Finite element method


External links

* [ The Finite Volume Method (FVM) - An introduction] by Oliver Rübenkönig of Albert Ludwigs University of Freiburg, available under the GFDL.

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