TY - GEN
T1 - Design of a scalable trailing edge of morphing wings
AU - Li, Bing
AU - Wang, Hefei
AU - Li, Gang
N1 - Publisher Copyright:
© 2014 IEEE.
PY - 2014/4/20
Y1 - 2014/4/20
N2 - A networking mechanism was designed based on scalable trailing edge to satisfy the requirements of morphing wings. By this way, we can increase the lift coefficient and the aerodynamic efficiency of the aircraft in the process of taking off and landing. We use Lagrange equations to set up the system dynamics model. Simulation results by Simulink and Fluent show that the whole system can realize the flexible curved transition and the system itself has good scalability. And it will have better improvement on the aerodynamic performance of the aircraft.
AB - A networking mechanism was designed based on scalable trailing edge to satisfy the requirements of morphing wings. By this way, we can increase the lift coefficient and the aerodynamic efficiency of the aircraft in the process of taking off and landing. We use Lagrange equations to set up the system dynamics model. Simulation results by Simulink and Fluent show that the whole system can realize the flexible curved transition and the system itself has good scalability. And it will have better improvement on the aerodynamic performance of the aircraft.
UR - https://www.scopus.com/pages/publications/84949928531
U2 - 10.1109/ROBIO.2014.7090694
DO - 10.1109/ROBIO.2014.7090694
M3 - 会议稿件
AN - SCOPUS:84949928531
T3 - 2014 IEEE International Conference on Robotics and Biomimetics, IEEE ROBIO 2014
SP - 2378
EP - 2382
BT - 2014 IEEE International Conference on Robotics and Biomimetics, IEEE ROBIO 2014
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 2014 IEEE International Conference on Robotics and Biomimetics, ROBIO 2014
Y2 - 5 December 2014 through 10 December 2014
ER -