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

Table 1

Parameters for a thin symmetrical airfoil.

	1.2254 kgs/m^3
	6.1272 kgs⋅m^2
	2563.83 N-m/Rad
	1962.433 N/m
	19.624 kgs
	1.829 m
	m
	−0.2