Monitoring Convergence

To determine when the problem has converged, plot the lift and drag coefficients.

Use the following steps:
  1. Right-click the Reports node and select New > Flow / Energy > Force Coefficient.
    A new report node named Force Coefficient 1 is created.
  2. Rename this node Drag Coefficient
  3. Select the Drag Coefficient node and set the following properties:
    Property Setting
    Reference Density 1.177 kg/m^3
    Reference Velocity 252 m/s
    Parts Regions > Overset 2D > Airfoil


  4. Right-click the Drag Coefficient node and select Create Monitor and Plot from Report.
    A new plot node appears named Drag Coefficient Monitor Plot.
  5. Create a lift coefficient report.
    1. Copy and paste the Drag Coefficient node onto the Reports node.
    2. Rename the new Drag Coefficient copy node to Lift Coefficient.
    3. Select the Lift Coefficient report and in the Properties dialog, set Direction to [0.0, 1.0, 0.0].
  6. Right-click the Lift Coefficient node and select Create Monitor and Plot from Report.
    A new plot node appears named Lift Coefficient Monitor Plot.
  7. Save the simulation.