Novel roll effector based on zero-mass-flux dual synthetic jets and its flight test  

作　　者：Zhenbing LUO Zhijie ZHAO Jiefu LIU Xiong DENG Mu ZHENG Hang YANG Qingyang CHEN Shiqing LI 

机构地区：[1]College of Aeronautics and Astronautics,National University of Defense Technology,Changsha 410073,China

出　　处：《Chinese Journal of Aeronautics》2022年第8期1-6,共6页中国航空学报（英文版）

基　　金：co-supported by the National Natural Science Foundation of China(Nos.11972369,11872374);the Youth Science and Technology Innovation Award Funded Project of National University of Defense Technology,China(No.434517314)。

摘　　要：The autonomous and controllable Dual Synthetic Jet Actuator(DSJA)is firstly integrated into the Unmanned Aerial Vehicle(UAV),and flight tests without the deflection of rudders are carried out to verify the viability of DSJA to control the attitudes of UAV during cruising.DSJA is improved into an actuator with two diaphragms and three cavities,which has higher energy levels.Actuators,differentially distributed on both sides of the wings,are installed on the trailing edge close to the wing tips.Flight tests,containing Differential Circulation Control(DCC)using double-side actuators,Positive Circulation Control(PCC)using left-side actuators and Negative Circulation Control(NCC)using right-side actuators,are implemented at cruising speed of 25 m/s.Results show that roll attitude control without rudders could be realized by DSJAs.DCC and NCC can generate the rightward roll and yaw angular velocity,prompting UAV to turn right.The stronger controlling ability can be achieved by DCC,with the maximum roll angular velocity of 15.62(°)/s.PCC can generate a rightward roll moment,but a leftward yaw moment will be produced at the same time.Leftward yaw induces the leftward rolling moment,which weakens the roll control effect,making UAV keep to yaw to the left with a small slope.

关 键 词：Active flow control Actuators with two diaphragms and three cavities Circulation control Dual synthetic jets Flight test Roll attitude control 

分 类 号：V217[航空宇航科学与技术—航空宇航推进理论与工程]