Author: John Singleton and Rajesh Bhaskaran
Problem Specification
1. Pre-Analysis & Start-Up
2. Geometry
3. Mesh
4. Setup (Physics)
5. Solution
6. Results
7. Verification and Validation
Exercises
Under Construction!!
5. Solution
Second Order Upwind Momentum Scheme
Solution > Solution Methods > Spatial Discretization. Set Momentum to Second Order Upwind
Convergence Criterion
Solution > Monitors > Residuals > Edit.... Set the Absolute Criteria for , x-velocity and y-velocity all to 1e-6. Click ok
Solution > Monitors > Drag > Edit.... Then check Print to Console and Plot. Next, click cylinderwall, which is located under Wall Zones. Lastly, click ok
Solution Initialization
Solution > Solution Initialization. Set Compute From to farfield1. Then, click Initialize.
Iterate Until Convergence
Solution > Run Calculation. Set the Number of Iterations to 2000. Then, click Calculate. (You may have to hit Calculate twice.) Now, have a cup of coffee.
Go to Step 6: Results
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