[ANSYS, Inc. Logo] return to home search
next up previous contents

Step 8: Solution

1.   Set the solution parameters.

figure Solution Methods

figure

(a)   Retain the default setting of Least Squares Cell Based for the Gradient in the Spatial Discretization group box.

(b)   Select Second Order Upwind from the Momentum and Energy drop-down lists.

2.   Set the solution controls.

figure Solution Controls

figure

(a)   Enter 0.9 for Energy in the Under-Relaxation Factors group box.

3.   Enable the plotting of residuals during the calculation.

figure Monitors figure figure Residuals figure Edit...

figure

(a)   Make sure Plot is enabled in the Options group box.

(b)   Click OK to close the Residual Monitors dialog box.

4.   Initialize the solution.

figure Solution Initialization

figure

(a)   Retain the default setting of 300 K for Temperature in the Initial Values group box.

(b)   Click Initialize.

  The values shown in the task pane will be used as the initial condition for the solution.

5.   Save the case file ( tubebank.cas).

File $\rightarrow$ Write $\rightarrow$ Case...

6.   Start the calculation by requesting 350 iterations.

figure Run Calculation

figure

(a)   Enter 350 for Number of Iterations.

(b)   Click Calculate.

  The energy residual curve that is displayed in the graphics window will begin to flatten out as it approaches 350 iterations. For the solution to converge to the recommended residual value of $10^{-6}$, you need to reduce the under-relaxation factor for energy.

7.   Change the Under-Relaxation Factor for Energy to 0.6.

figure Solution Controls

8.   Continue the calculation by requesting another 300 iterations.

figure Run Calculation

  After restarting the calculation, the plot of the energy residual will display an initial dip as a result of the reduction of the under-relaxation factor. The solution will converge in a total of approximately 580 iterations.

9.   Save the case and data files ( tubebank.cas and tubebank.dat).

File $\rightarrow$ Write $\rightarrow$ Case & Data...


next up previous contents Previous: Step 7: Boundary Conditions
Up: Modeling Periodic Flow and
Next: Step 9: Postprocessing
Release 12.0 © ANSYS, Inc. 2009-02-09