Proper Orthogonal Decomposition as Surrogate Model for Aerodynamic Optimization

Table 2

NACA 0012 airfoil. List of the reconstruction combinations.

Reconstruction point	Mach number	[°
A	0.17	2.5
B	0.12	4.5
C	0.08	3.5
D	0.25	1.5
E	0.05	4.5
F	0.23	4.7
G	0.21	3.7