Fig.1

Basics of circulation control aerodynamics［1］

Fig.2

FAST-MAC model［27］

Fig.3

Time line of demonstrator aircraft developed for flight evaluation of fluidic control effectors ［36］

Fig.4

Coanda influence on streamlines［17］

Fig.5

Equivalence of circulation control via trailing edge flap and trailing edge blowing［36］

Fig.6

Internal structure of 17% supercritical GACC airfoil with circular trailing edge of 2%［17］

Fig. 7

Influence of steady jet on lift with different momentum coefficients of GACC airfoil ［17］

Fig.8

Coanda effect with different momentum coefficients with 0°angle of attack［17］

Fig.9

Hydrogen bubble flow visualization of airfoil［17］

Fig.10

Lift characteristics of 2-D GACC airfoil［17］

Fig.11

Lift performance of GACC 2-D airfoil negative lift configuration （lower surface blowing，α=0°） ［17］

Fig.12

Drag polar for GACC 2-D airfoil negative lift configuration（lower surface blowing，α=0°）［17］

Fig.13

Lift and drag performance of GACC airfoil at different velocity ratios［17］

Fig.14

Aircraft fluidic control schemes［40］

Fig.15

Wing profiles and 3-D view of SACCON UCAV configuration［92］

Fig.16

Schematic view of trailing edge circulation control configuration［94］

Fig.17

Pitch， roll and yaw moment coefficients with respect to blowing at inboard of left wing （IBC）［40］

Fig.18

Difference in pitch， roll and yaw moment coefficients due to different control effectors［40，95-96］

Fig.19

Demon UAV［105］

Fig.20

MAGMA UAV［39］

Fig.21

ICE vehicle［106］

Fig.22

Tailless flying wing unmanned flight aircraft［91］

Fig.23

Demonstrator for flight control using jet［90］

Fig.24

Flying wing UAV［84］

Fig.25

MAGMA fluidic systems architecture［38］

Fig.26

APU/compressor installation［105］

Fig.27

Turbojet engine and bleed system［91］

Fig.28

Shape of circulation control actuator［91］

Fig.29

Design space for circulation control device［41］

Fig.30

Original flight control system

Fig.31

Fluidic flight control system