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Zienkiewicz O.C., Taylor R.L. Vol. 3. The finite - tiera.ru

Zienkiewicz O.C., Taylor R.L. Vol. 3. The finite - tiera.ru

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154 Free surfaces, buoyancy and turbulent incompressible ¯ows<br />

evaluated. <strong>The</strong>se may on occasion be the only driving force of the problem. In this<br />

situation it is convenient to note that the body force with constant density can be<br />

considered as balanced by an initial hydrostatic pressure and thus the driving force<br />

which causes the motion is in fact the body force caused by the di€erence of local<br />

density values. We can thus write the body force at any point in the equations of<br />

motion (4.2) as<br />

@ui @<br />

‡ …u<br />

@t @x<br />

jui† ˆÿ<br />

j<br />

@p<br />

‡<br />

@xi @ ij<br />

ÿ g<br />

@x<br />

i… ÿ 1† …5:8†<br />

j<br />

where is the actual density applicable locally and 1 is the undisturbed constant<br />

density. <strong>The</strong> actual density entirely depends on the coe cient of thermal expansion<br />

of the ¯uid as compressibility is by de®nition excluded. Denoting the coe cient of<br />

thermal expansion as T, we can write<br />

1<br />

T ˆ<br />

@<br />

@T<br />

…5:9†<br />

where T is the absolute temperature. <strong>The</strong> above equation can be approximated to<br />

T<br />

1 ÿ 1<br />

T ÿ T1 …5:10†<br />

Replacing the body force term in the momentum equation by the above relation we<br />

can write<br />

@ui @<br />

‡ …u<br />

@t @x<br />

jui† j<br />

ˆÿ @p<br />

‡<br />

@xi @ ij<br />

‡<br />

@xj Tgi…T 1 ÿ T† …5:11†<br />

For perfect gases, we have<br />

ˆ p<br />

…5:12†<br />

RT<br />

and here R is the universal gas constant. Substitution of the above equation (assuming<br />

negligible pressure variation) into Eq. (5.9) leads to<br />

T ˆ 1<br />

…5:13†<br />

T<br />

<strong>The</strong> various governing non-dimensional numbers used in the buoyancy ¯ow<br />

calculations are the Grasho€ number (for a non-dimensionalization procedure see<br />

references 24, 25)<br />

and the Prandtl number<br />

Gr ˆ g T…T 1 ÿ T†L 3<br />

…5:14†<br />

Pr ˆ …5:15†<br />

where L is a reference dimension, and and are the kinematic viscosity and thermal<br />

di€usivity respectively and are de®ned as<br />

ˆ ; ˆ k<br />

cp …5:16†

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