title: Aerodynamic performance due to forewing and hindwing interaction in gliding dragonfly flight.
abstract: Aerodynamic performance due to forewing and hindwing interaction in gliding dragonfly flight has been studied using a multiblock lattice Boltzmann method. We find that the interactions between forewing and hindwing effectively enhance the total lift force and reduce the drag force on the wings compared to two independent wings. The interaction mechanism may be associated with the triangular camber effect by modulating the relative arrangement of the forewing and hindwing. The results obtained in this Brief Report provide physical insight into the understanding of aerodynamic behaviors for gliding dragonfly flight.
authors: Department of Modern Mechanics, University of Science and Technology of China, Anhui, Hefei 230026, China.
authors: Jie
authors: J
authors: Zhang
authors: Xi-Yun
authors: XY
authors: Lu