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FLOW AROUND A CYLINDER - istiarto

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4.5.3 Outflow boundary<br />

– 4.32 –<br />

Suppose that the outflow lies at the east face of the boundary cell P (see Fig. 4.7). Across<br />

the outflow face, the convective flux is computed according to the upwinding principle of<br />

Eq. 4.28:<br />

C � ��1 � ��1<br />

�F � � q<br />

�� e e �P � qout �P<br />

while the diffusion flux is set to zero:<br />

F D � � � 0<br />

e<br />

leading to a simplified form of Eq. 4.43:<br />

��<br />

F � ��1<br />

e � qout �P<br />

�<br />

where<br />

��<br />

qout is either imposed or computed from the upwinding of P value at the former<br />

iteration step:<br />

��<br />

q �<br />

�<br />

out � Vout<br />

�<br />

�Se � VP � Se<br />

The same upwinding process finds the other variables at the boundary node E.<br />

� E � � e � � P<br />

Momentum and k-� equations<br />

Fig. 4.7 Outflow boundary.<br />

� set all coefficients related to node E in Eq. 4.52 to zero:<br />

C D C D<br />

aE � aE � a P<br />

� � ��a E P�<br />

� b<br />

E D � � � b<br />

E 1D � � � b<br />

E 2D � � � 0<br />

E

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