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Diploma report Implementation and verification of a simple ... - LPAS

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have<br />

∫<br />

d z2<br />

∫ x2<br />

ρ(x, z, t)dxdz = F 1 (z, t) − F 2 (z, t) + G 1 (x, t) − G 2 (x, t), (6)<br />

dt z 1 x 1<br />

where F i (z, t) are the flux functions at the lateral boundaries x i , i = 1, 2, <strong>and</strong> G i (x, t) the<br />

fluxes at the top <strong>and</strong> bottom boundaries z i , i = 1, 2. Note that F 1 (z, t) corresponds to the<br />

flux to the right <strong>and</strong> −F 2 (z, t) represents the flux to the left.<br />

Equation (6) represents the integral from <strong>of</strong> a conservation law for the mass <strong>and</strong> the<br />

flux functions are to be related to ρ(x, z, t) in order to obtain an equation that might be<br />

solvable for ρ. The mass flux through boundary x i is associated with the mass transported<br />

with velocity u through x i so that F is given by ρu. Similarly, G is given by ρw. The integral<br />

form <strong>of</strong> the conservation law becomes then<br />

d<br />

dt<br />

∫ z2<br />

∫ x2<br />

z 1<br />

x 1<br />

ρ(x, z, t)dxdz = −ρu∣ x 2<br />

− ρw∣ z 2<br />

. (7)<br />

x 1 z 1<br />

Assuming that ρ, u <strong>and</strong> w are smooth functions, the integral form <strong>of</strong> the conservation law can<br />

be transformed into a partial differential equation (see appendix A). The differential form <strong>of</strong><br />

the conservation law for ρ is then<br />

ρ t + (ρu) x + (ρw) z = 0. (8)<br />

This equation called the continuity equation models the conservation <strong>of</strong> mass.<br />

In addition to ρ(x, z, t), the velocity components u(x, z, t) <strong>and</strong> w(x, z, t) are also to be determined<br />

<strong>and</strong> two equations are needed for this. The velocities themselves are not conserved<br />

quantities, but the x-momentum ρu <strong>and</strong> the z-momentum ρw are. Each <strong>of</strong> these momenta<br />

are transported with the flow <strong>and</strong>, by analogy with the density flux in (8), this will give<br />

contributions <strong>of</strong> ((ρu)u) x + ((ρu)w) z <strong>and</strong> ((ρw)u) x + ((ρw)w) z to the x- <strong>and</strong> z-momentum<br />

respectively. Beside this, there are additional microscopic terms for the momentum fluxes<br />

that are due to the pressure in the fluid. These microscopic fluxes are caused by the fact that<br />

all nearby molecules are not moving at the same speed in a gas. Pressure variation in the<br />

x-direction, measured by p x appears in the equation for ρu, while p z appears in the equation<br />

for ρw.<br />

In the vertical direction, there are external gravity forces acting on the gas that accelerate<br />

downward individual molecules. These forces must be integrated over the domain<br />

<strong>and</strong> this contribution added to the integral conservation law for z-momentum (if z is aligned<br />

with the gravitational acceleration). Thus the differential form <strong>of</strong> the z-momentum equation<br />

will contain a source term <strong>of</strong> s = −ρ∇Φ, where Φ = gz is the gravitational potential.<br />

The differential forms <strong>of</strong> the conservation laws for momentum are then<br />

(ρu) t + (ρu 2 + p) x + (ρuw) z = 0, (9)<br />

(ρw) t + (ρwu) x + (ρw 2 + p) z = −ρ∇Φ. (10)<br />

6

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