Research Article

Nonlinear Unsteady Aerodynamics Reduced Order Model of Airfoils Based on Algorithm Fusion and Multifidelity Framework

Table 4

Training cases in convergence analysis.

Training group numberVelocity intervals (m/s)Velocity in groups (m/s)

15010, 60
22510, 35, 60
31010, 20, 30, 40, 50, 60
4510, 15, 20, 25, 30, 35, 40, 45, 50, 55, 60