Corrigendum to: Discussion on "Active aeroelastic control of 2-D wing-flap systems operating in an incompressible flowfield and impacted by a blast pulse" by Librescu et al., Journal of Sound and Vibration 283 (3–5) (2005) 685–706 [Journal of Sound Vibration 332 (13) (2013) 3351–3358]

Flutter of wings involving a locally distributed flexible control surface

“…They obtained the model by invoking Jones' exponential approximation of Wagner's indicial loading function and Laplace transform of the airload expressions. Also, through an alternative integro-differential scheme [12], York [13] developed another state-space model of the same airfoil-aileron configuration, requiring subsequent corrections which have been recently discussed by Mozaffari-Jovin et al [14,15]. Many scholars have adopted these two state-space models for linear and nonlinear flutter analyses as well as in the design of active control systems for flutter suppression and atmospheric turbulence alleviation.…”