The nonlinear equations for coupled elastic flapping-twisting motion of a dragonfly-inspired smart flapping wing are used for a flapping wing actuated from the root by a PZT unimorph in the piezofan configuration.Exci...The nonlinear equations for coupled elastic flapping-twisting motion of a dragonfly-inspired smart flapping wing are used for a flapping wing actuated from the root by a PZT unimorph in the piezofan configuration.Excitation by the piezoelectric harmonic force generates only the flap bending motion,which,in turn,induces the elastic twist motion due to interaction between flexural and torsional vibration modes.An unsteady aerodynamic model is used to obtain the aerodynamic forces.Numerical simulations are performed using a wing whose size is the same as the dragonfly Sympetrum frequens wing.It is found that the value of average lift reaches its maximum when the smart flapping wing is excited at a frequency closer to the natural frequency in torsion.Moreover,consideration of the elastic twisting of the flapping wing leads to an increase in the lift force.It is also found that the flapping wing generates sufficient lift to support its own weight and carry a small payload.Therefore,the piezoelectrically actuated smart flapping wing based on the geometry of a Sympetrum frequens wing and undergoing flapping-twisting motions can be considered as a potential candidate for use in micro air vehicle applications.展开更多
文摘The nonlinear equations for coupled elastic flapping-twisting motion of a dragonfly-inspired smart flapping wing are used for a flapping wing actuated from the root by a PZT unimorph in the piezofan configuration.Excitation by the piezoelectric harmonic force generates only the flap bending motion,which,in turn,induces the elastic twist motion due to interaction between flexural and torsional vibration modes.An unsteady aerodynamic model is used to obtain the aerodynamic forces.Numerical simulations are performed using a wing whose size is the same as the dragonfly Sympetrum frequens wing.It is found that the value of average lift reaches its maximum when the smart flapping wing is excited at a frequency closer to the natural frequency in torsion.Moreover,consideration of the elastic twisting of the flapping wing leads to an increase in the lift force.It is also found that the flapping wing generates sufficient lift to support its own weight and carry a small payload.Therefore,the piezoelectrically actuated smart flapping wing based on the geometry of a Sympetrum frequens wing and undergoing flapping-twisting motions can be considered as a potential candidate for use in micro air vehicle applications.
