Control Application of Piezoelectric Materials to Aeroelastic Self-Excited Vibrations

Table 1

Aerodynamic force coefficients of the typical aeroelastic case.

	𝐶𝑖(1,1)	𝐶𝑖(1,2)	𝐶𝑖(2,1)	𝐶𝑖(2,2)
𝐶0	32.8508	38.0274	−6.3067	11.1821
𝐶1	1.7196	1.0004	0.2946	−0.2616
𝐶2	2.9262	0.1211	−0.1329	−0.4225
𝐶3	−3.2556	−2.0932	10.5449	−0.8498
𝐶4	26.2369	60.9038	−6.0006	16.9342
𝐶5	0.7657	−6.9970	2.0261	−5.1781
𝐶6	−6.8888	30.7360	−0.3372	8.1604