Uncertainty Quantification and Bifurcation Analysis of an Airfoil with Multiple Nonlinearities

Table 4

The optimization results obtained by the proposed method.

Variables	Case 1	Case 2	Case 3
𝑘𝜉	15	—	22.9059
𝑘𝛼	—	15	15
𝑄	2.3277	4.0802	3.6036
𝜔	0.8533	0.5982	0.7193