Uncertainty Quantification and Bifurcation Analysis of an Airfoil with Multiple Nonlinearities

Table 5

The nonlinear equality and inequality constraints at these optimal solutions.

Constraints	Case 1	Case 2	Case 3
𝐠(𝐔,𝜔)	3.7954𝑒−13	2.2204𝑒−16	2.2438𝑒−12
𝜌1	1.0000	1.0000	1.0000
𝜌2	1.0000	1.0000	1.0000
𝜌3,𝜌4	0.1660±0.2292𝑖	0.1542±0.0592𝑖	0.1359±0.1777𝑖
max(|𝝆|)	1.0000	1.0000	1.0000