Designing a Control System for an Airplane Wing Flutter Employing Gas Actuators

Table 2

Parameters for a thin symmetrical airfoil from [7].

	1.2254 kgs/m^3
	0.1065 kgsm^2
	Nonlinear N-m/Rad
	2844.4 N/m
	12.287 kgs
	0.27 m
	m