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Basics of Fluid Mechanics, 2014a

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246 CHAPTER 8. DIFFERENTIAL ANALYSIS<br />

after rearrangement equations such as (8.57) and (8.58) transformed into<br />

internal forces<br />

{ }} {<br />

DU x<br />

Dt ρ ✚✚dx dy ✚dz =<br />

surface forces<br />

{( }} {<br />

∂τxx<br />

∂x<br />

+ ∂τ yx<br />

∂y<br />

+ ∂τ )<br />

zx<br />

✚✚dx<br />

∂z dy ✚dz +<br />

body forces<br />

{ }} {<br />

f Gx ρ✚✚dx dy ✚dz (8.61)<br />

equivalent equation (8.61) fory coordinate is<br />

ρ DU y<br />

Dt<br />

The same can be obtained for the z component<br />

ρ DU z<br />

Dt<br />

=<br />

=<br />

(<br />

∂τxy<br />

∂x + ∂τ yy<br />

∂y<br />

+ ∂τ )<br />

zy<br />

+ ρf Gy (8.62)<br />

∂z<br />

(<br />

∂τxz<br />

∂x + ∂τ yz<br />

∂y<br />

+ ∂τ )<br />

zz<br />

+ ρf Gz (8.63)<br />

∂z<br />

Advance material can be skipped<br />

Generally the component momentum equation is as<br />

ρ DU i<br />

Dt<br />

=<br />

(<br />

∂τii<br />

∂i<br />

+ ∂τ ji<br />

∂j + ∂τ )<br />

ki<br />

+ ρf Gi (8.64)<br />

∂j<br />

End Advance material<br />

Where i is the balance direction and j and k are two other coordinates. Equation<br />

(8.64) can be written in a vector form which combined all three components into one<br />

equation. The advantage <strong>of</strong> the vector from allows the usage <strong>of</strong> the different coordinates.<br />

The vector form is<br />

ρ DU<br />

Dt = ∇·τ (i) + ρf f G (8.65)<br />

where here<br />

τ (i) = τ ix î + τ iy ĵ + τ iẑk<br />

is part <strong>of</strong> the shear stress tensor and i can be any <strong>of</strong> the x, y, or z.<br />

Or in index (Einstein) notation as<br />

ρ DU i<br />

Dt<br />

= ∂τ ji<br />

∂x i<br />

+ ρf Gi (8.66)<br />

End Advance material<br />

Equations (8.61) or(8.62) or(8.63) requires that the stress tensor be defined<br />

in term <strong>of</strong> the velocity/deformation. The relationship between the stress tensor and<br />

deformation depends on the classes <strong>of</strong> materials the stresses acts on. Additionally, the<br />

deformation can be viewed as a function <strong>of</strong> the velocity field. As engineers do in general,<br />

the simplest model is assumed which referred as the solid continuum model. In this<br />

model the relationship between the (shear) stresses and rate <strong>of</strong> strains are assumed to be

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