Numerical Investigation of Flapwise-Torsional Vibration Model of a Smart Section Blade with Microtab

Table 1

Eigenvalues for structural and aeroelastic models with  m/s and .

	Present model	Kallesøe [20]
Structural model	−0.0010 ± 0.1087; (); Hz	Hz
	−0.0002 ± 0.0162; (); Hz	Hz
Aeroelastic model	−0.002 ± 0.1071; (); Hz	Hz
	−0.004 ± 0.0151; (); Hz	Hz