Research on Adaptive Flexible Wing with Variable Trailing Edge

Abstract The trailing edge deformable wing is one of the main development directions future aircraft design. technology active camber can significantly improve aerodynamic performance aircraft. In this paper, motor drives parabolic crankshaft and distributed flexible skin wing, which realize deflection at a large angle 0~30 degrees. At same time, surface continuous smooth. Moreover, simulation results deformed show that beneficial to increase lift. It maximum lift coefficient by 2 times drag ratio 18%. Adaptive applied rocket sleds with side wings. This downward pressure block operation safety.