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FLOW AROUND A CYLINDER - istiarto

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– 4.5 –<br />

The volume integrals of the convective and diffusive terms, the second and third terms on<br />

the left-hand side, can be expressed as integral over the closed surface bounding the<br />

control volume by applying Gauss divergence theorem (Versteeg and Malalasekera,<br />

1995, p. 26; Hirsch, 1988, p. 241):<br />

�<br />

�� �t<br />

���<br />

� �dV �<br />

V<br />

�� ��V� dS � �<br />

S<br />

S ��� ��dS<br />

�� � ��� R�dV (4.15)<br />

where S is the surface vector normal outward to the control volume dV .<br />

�� � ��<br />

�� ��<br />

�� Table 4.2 Terms in the general transport equation, Eq. 4.13.<br />

��� �� � t � � � � �V��<br />

��� ��� ���<br />

R� (4.13)<br />

��<br />

R �<br />

1 u �t � 1 �p �<br />

�<br />

� �x �x � ��<br />

�� t<br />

2 v �t � 1 �p �<br />

�<br />

� �y �x � ��<br />

t<br />

��<br />

��<br />

3 w �t � 1 �p �<br />

�<br />

� �z �x � ��<br />

�� t<br />

4 1 0 0<br />

5 k � t � k G-��<br />

6 �� � t � � c 1<br />

4.2 Solution strategy: the iterative method<br />

V<br />

�u��<br />

�<br />

�<br />

�x �� �y � �� �v��<br />

�<br />

�� t �<br />

�x��<br />

�z � �� �w��<br />

�� t<br />

�x �� � gx �u��<br />

�y ��<br />

��� �<br />

�y � �� �v��<br />

t<br />

��<br />

��<br />

�y��<br />

��� �<br />

�z � �� �w��<br />

t<br />

��<br />

��<br />

�y ��<br />

��� gy �u��<br />

�<br />

�<br />

�z �� �y � �� �v��<br />

�<br />

�� t �<br />

�z��<br />

�z � �� �w��<br />

�� t<br />

�z �� � gz �<br />

k G � c �<br />

2<br />

k �<br />

The integral form of the general transport equation, Eq. 4.15, is used to obtain the<br />

solution for u, v, w, k, and � by substituting these variables to the scalar variable �. The<br />

solution of the equation is sought at discrete time steps; calculations are performed at<br />

every discrete time steps and repeated until a steady-state solution is obtained. The time<br />

derivative term in Eq. 4.15 facilitates the application of the model to transient flow<br />

problems; in this case, the solution at each discrete time step must converge. When the<br />

problems concern steady case ones —as is the case in the present work— the time<br />

derivative serves as an iteration loop. In this case the solution at each time step is<br />

considered as an intermediate solution, and the end-solution (the steady-state one) is<br />

obtained when all variables �‘s converge. Since the end-solution that is sought, it is not<br />

necessary to force the intermediate solution to converge at the same degree of<br />

convergence as that of the end-solution. The complete computational procedure is<br />

depicted in the flowchart shown in Fig. 4.1. The time loop, from the initial until the

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