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

Figure 17

Prediction of lift coefficients of test cases: (a) inlet velocity is 100 m/s, (b) inlet velocity is 150 m/s, (c) inlet velocity is 200 m/s, and (d) inlet velocity is 250 m/s.

(a) 100 m/s

(b) 150 m/s

(c) 200 m/s

(d) 250 m/s