1. Piston theory – a new aerodynamic tool for the aeroelastician;Ashley;Journal of the Aerospace Sciences,1956
2. Non-linear adaptive model free control of an aeroelastic 2-D lifting surface;Behal;AIAA Journal of Guidance, Control, and Dynamics,2006
3. E.J. Breitbach, Effects of structural non-linearities on aircraft vibration and flutter, AGARD TR-665, North Atlantic Treaty Organization, Neuilly sur Seine, France, January 1978
4. Wing Theory in Supersonic Flow;Carafoli,1969
5. Unsteady unified hypersonic/supersonic method for aeroelastic applications including wave/shock interaction;Chavez;AIAA Journal,1995