TY - JOUR
T1 - Active Flow Control Based on Plasma Synthetic Jet for Flapless Aircraft
AU - Wang, Xin
AU - Yan, Jie
AU - Dhupia, Jaspreet Singh
AU - Zhu, Xiaosong
N1 - Publisher Copyright:
© 2013 IEEE.
PY - 2021
Y1 - 2021
N2 - Active flow control (AFC) based on plasma synthetic jet actuator (PSJA) has been attracted a lot of researchers since Anderson and Knight put forward the concept of PSJA for the first time. Since then the characteristic of PSJA has been studied by means of many numerical simulations and experiments. This article showed a series of studies that manipulated a vehicle without moving control surfaces. Firstly, we research the characteristics of the aviation actuator, including the effects of structure and parameters on performance. Secondly, we explore the influence of the actuator on the air field around the aircraft by simulation, including the influence of the actuator on the aerodynamic coefficients and pitching moment coefficient. Finally, since these changes are similar to those caused by the deflection of the rudder surface, we can equivalent the effect of the PSJA to the deflection of the rudder surface, and simulate the three-degree-of-freedom pitch control channel of the aircraft to illustrate the effectiveness of PSJA on the flapless control system.
AB - Active flow control (AFC) based on plasma synthetic jet actuator (PSJA) has been attracted a lot of researchers since Anderson and Knight put forward the concept of PSJA for the first time. Since then the characteristic of PSJA has been studied by means of many numerical simulations and experiments. This article showed a series of studies that manipulated a vehicle without moving control surfaces. Firstly, we research the characteristics of the aviation actuator, including the effects of structure and parameters on performance. Secondly, we explore the influence of the actuator on the air field around the aircraft by simulation, including the influence of the actuator on the aerodynamic coefficients and pitching moment coefficient. Finally, since these changes are similar to those caused by the deflection of the rudder surface, we can equivalent the effect of the PSJA to the deflection of the rudder surface, and simulate the three-degree-of-freedom pitch control channel of the aircraft to illustrate the effectiveness of PSJA on the flapless control system.
KW - active flow control
KW - flapless control system
KW - Plasma synthetic jet actuator
UR - http://www.scopus.com/inward/record.url?scp=85098779043&partnerID=8YFLogxK
U2 - 10.1109/ACCESS.2020.3016342
DO - 10.1109/ACCESS.2020.3016342
M3 - 文章
AN - SCOPUS:85098779043
SN - 2169-3536
VL - 9
SP - 24305
EP - 24313
JO - IEEE Access
JF - IEEE Access
M1 - 9166482
ER -