Page 257 - Finite Element Analysis with ANSYS Workbench

248 Chapter 12 Compressible Flow Analysis

(e) Solving for Solution

 In the Solution Methods under Solution, be sure to select
Second Order Upwind under Spatial Discretization.

 In the Solution Controls under Solution, ensure that the
Courant Number is set to 5.
 In the Monitors under Solution, select Residuals - Print,
Plot and double-click on Edit button. Then, change the
Convergence Absolute Criteria to 1e-6, and click OK.

 In the Solution Initialization under Solution, select Stan-
dard Initialization. Also select farfield from the drop-
down box under Compute from, and click Initialize
button.