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

Table 1

Information of cases.

Case number	Case 1	Case 2	Case 3	Case 4	Case 5	Case 6
Inlet Mach number	0.059	0.118	0.120	0.300	0.300	0.300
Reduced frequency	0.460	0.230	0.124	0.100	0.100	0.100
chord length (m)	1.0	1.0	0.55	0.4064	0.4064	0.4064
Initial angle of attack(°)	0	0	15	5	10	15
Amplitude of motion (°)	10	10	10	10	10	10