TY - GEN
T1 - Numerical analysis of blowing and suction about two-dimensional airfoil
AU - Li, Biaoquan
AU - Wang, Zhengjie
AU - He, Shun
AU - Guo, Shijun
N1 - Publisher Copyright:
© 2019 IEEE.
PY - 2019/10
Y1 - 2019/10
N2 - The Flapless Air Vehicle is a major direction for the development of unmanned systems in the future due to its simple structure and convenient operation. In this paper, the characteristics of the Flapless Air Vehicle are introduced and the features of Fluidic Control technology are also presented. For future design of Flapless Air Vehicle, this paper makes some simulation analysis on the Fluidic Control technology's blowing and suction control scheme. Different types of air blowing and suction are analyzed and the influence of different positions and different flow rates on the lift and drag coefficient of the wing are presented. The results of the simulation show that the selection of suitable blowing and suction conditions on the wing can increase the lift and reduce the drag. By simple blowing and suction control, the aircraft can achieve self-generated flight control. All of these calculations will be helpful in the design of a flapless aircraft.
AB - The Flapless Air Vehicle is a major direction for the development of unmanned systems in the future due to its simple structure and convenient operation. In this paper, the characteristics of the Flapless Air Vehicle are introduced and the features of Fluidic Control technology are also presented. For future design of Flapless Air Vehicle, this paper makes some simulation analysis on the Fluidic Control technology's blowing and suction control scheme. Different types of air blowing and suction are analyzed and the influence of different positions and different flow rates on the lift and drag coefficient of the wing are presented. The results of the simulation show that the selection of suitable blowing and suction conditions on the wing can increase the lift and reduce the drag. By simple blowing and suction control, the aircraft can achieve self-generated flight control. All of these calculations will be helpful in the design of a flapless aircraft.
KW - Flapless Air Vehicle
KW - Flow blowing
KW - Flow suction
KW - Fluidic Control technology
KW - lift and drag coefficient
UR - http://www.scopus.com/inward/record.url?scp=85080935666&partnerID=8YFLogxK
U2 - 10.1109/ICUS48101.2019.8996032
DO - 10.1109/ICUS48101.2019.8996032
M3 - Conference contribution
AN - SCOPUS:85080935666
T3 - Proceedings of the 2019 IEEE International Conference on Unmanned Systems, ICUS 2019
SP - 195
EP - 199
BT - Proceedings of the 2019 IEEE International Conference on Unmanned Systems, ICUS 2019
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 2019 IEEE International Conference on Unmanned Systems, ICUS 2019
Y2 - 17 October 2019 through 19 October 2019
ER -