Fig.1

Classification of flow control technologies

Fig.2

Number of SCI and EI papers on the four most active flow control technology［15］

Fig.3

Piezoelectric synthetic jet and flow field［28］

Table 1

Influence of excitation parameters on delay phase angle［25］

Fig.4

Numerical simulation results of synthetic jet

Fig.5

In-phase enhancement mechanism and experimental flow field［25］

Fig.6

Reverse phase vector deflection and experimental flow field［25，36］

Fig.7

Self-support phenomenon［41］

Fig.8

Variation trend of jet normalized stroke with Stk［41］

Fig.9

Theoretical system of double synthetic jets

Fig.10

Dual synthetic jets and experimental flow field［25-26］

Fig.11

Vector dual synthetic jets control and effect［25，42］

Table 2

Comparison between dual synthetic jets and synthetic jet

Fig.12

Dual synthetic jets circulation control deviceand its control effect［46］

Fig.13

Flight test validation［47］

Fig.14

Change of flow field structure before and after control［52］

Fig.15

Rudder efficiency enhanced flight validation［52］

Fig.16

Vortex system reconstructed by leading-edge dual synthetic jets［60-61］

Fig.17

Reverse jet control based on dual synthetic jets［68-69］

Fig.18

Change of flow field before and after reverse jet control［68-69］

Fig.19

Aerodynamic stability augmentation technology［70］

Fig.20

Lift response changes before and after control［71］

Fig.21

Vectoring control of a primary jet using synthetic jet/dual synthetic jets

Fig.22

Three-flow thrust vector control technology［77］

Fig.23

Three flow thrust vector nozzles and experimental results

Fig.24

Three-flow thrust vectoring UAV and flight tests

Fig.25

Schematic diagram of three-axis attitude control for fixed wing UAV［88］

Fig.26

Flight test results of fixed wing UAV［88］

Fig.27

Schematic diagram of three-axis attitude control for flying wing UAV［89］

Fig.28

Flight test results of flying wing UAV［89］

Fig.29

Dual synthetic jets anti-icing technology［95］

Fig.30

Dual synthetic jets anti-icing technology of rotating platform［96］

Fig.31

Thermal synthesis dual jet defrosting and deicing［97］

Fig.32

Integrated anti-icing/flow control

Fig.33

Active and passive heat dissipation device［102］

Fig.34

Vector dual synthetic jets heat dissipationmethod［42，103-104］

Fig.35

Combined spray jet cooling device［105-106］

Fig.36

Spray cooling device［107］

Fig.37

Integrated vector spray jet device［108］

Fig.38

Active heat pipe［109］

Fig.39

Active liquid cooling cooling device［110］

Fig.40

Active liquid cooling experiment platform［111］

Fig.41

Comparison of nanoparticle distribution before and after actuator operation［116］

Fig.42

Thrust change curves with frequency［117］

Fig.43

Underwater flow field results of miniaturized actuator

Table 3

Characteristics and application of DSJ and efficiency enhancement in aeronautical technology