Static Aeroelastic Modeling and Rapid Analysis of Wings in Transonic Flow

Table 5

The sampling data of Mach number and angle of attack.

Mach number	Angle of attack (°)
0.7699	2.047
0.7293	1.638
0.7876	3.024
0.8158	1.208
0.8385	3.553
0.7469	2.739