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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
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 continuity, x-velocity and y-velocity to 1e-6. Click ok
Solution > Monitors > Create > Drag
Then check Print to Console and Plot. Next, click cylinderwall, which is located under Wall Zones. Lastly, click ok
Initial Guess
Solution > Solution Initialization > Standard Initialization.
Set Compute From to farfield1. Alternately, you can simply set X Velocity to 1 m/s. 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. The solution should converge after approximately 1600 iterations.
Save Project
Go to Step 6: Results
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