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Solution > Solution Methods > Spatial Discretization.
Set Momentum to Second Order Upwind

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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

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Solution > Solution Initialization.
Set Compute From to farfield1. Alternately, you can simply set X Velocity to 1 m/s. Then, click Initialize.

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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 1414 iterations.

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