The Use of Gramian Matrices for Aeroelastic Stability Analysis

Table 2

Reduced frequencies for the case study AGARD wing 445.6.

10^−3	2.10^−3	5.10^−3	10^−2
5.10^−2	0.1	0.2	0.3
0.5	0.6	0.8	1.0
1.5	2.0	3.0	4.0