Research Article
Time-Dependent Effects of Glaze Ice on the Aerodynamic Characteristics of an Airfoil
Table 1
Discretization error for iced airfoil in a transient simulation.
| Simulation type | Transient (2D) |
| Criteria parameter | Lift coefficient () | The number of elements in the mesh | 0.41, 1.7, 3.9 | The refinement factor | 1.32, 1.61 | The relative error (%) | 40, 2 | Numerical uncertainty in the fine grid solution (GCI) (%) | |
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