Investigating the effects of ionic polymer metal composite patches on aeroelastic characteristics of a cantilever wing in supersonic flow

This work presents energy harvesting from the limit cycle oscillation of fllow aspect ratio rectangular cantilever wings in supersonic flow. the wing is modeled according to the classical plate theory with von-karman strain-displacement relations for modeling large deections due to mid-plane stretching. the aerodynamic pressure is evaluated based on the quasi-steady first-order piston theory. linear and nonlinear aeroelastic characteristics of the considered model are accurately examined and the effects of ionic polymer metal composite (ipmc) energy harvesting on utter margin and limit cycle oscillation amplitudes are investigated. it is shown that the position of ipmc onthe wing has a great effect on the amount of harvested power. since ipmc induces a high level of strain, it produces the static deection of the wing. this static deection produces stiffness hardening of the entire system, and, accordingly, can greatly reduce the amplitude of limit cycle oscillation. obtained results show that the ipmc actuator has more influence on the limit cycle oscillation of the wing, while its effect on utter instability is negligible.