Fig.1

Different flow patterns for ventilated partial cavitating flows［4］

Fig.2

Flow pattern diagram changing with Eu and Qv［6］

Fig.3

Fitting envelope surface for ventilated cavity coalescence［7］

Fig.4

Ventilation cavitation flow pattern［8］

Fig.5

Distribution of mean value and uncertainty bars of mean surface pressure along length direction of vehicle （1 000 samples）［16］

Fig.6

Relationship between shedding frequency of ventilated cavitation and angle of attack［21］

Fig.7

Position of cavity break-off at different angles of attack［23］

Fig.8

Three-dimensional gas film fusion evolution process with different Froude numbers［28］

Fig.9

Parallel double-hole ventilation process on vehicle shoulder［30］

Fig.10

Bubble characteristic diagram under different initial pressures［30］

Fig.11

Relationship between dimensionless length of water layer and Froude number［30］

Fig.12

Comparison of cavity shape with and without groove at different ventilation rates［39］

Fig.13

Effect of surfactant on flow characteristics of tail cavity［58］

Fig.14

Tail cavitation evolution process based on ejection model［59］

Fig.15

Transient pressure variation law of vehicle tail

Fig.16

Pressure change during tail cavity shrinking process with different initial pressure［71］

Fig.17

Pressure oscillation on wet surface caused by tail cavity［72］

Fig.18

Track of head of slender body of water-exit at different launch angles［77］

Fig.19

T-S wavy vortex structure on cavity surface［84］

Fig.20

Pressure change law of measuring points during water-exit process of different head-shaped vehicles［96］

Fig.21

Comparison of load coefficient changes for different head shapes［97］

Fig.22

Comparison of deflection angles of bionic model and prototype in water-exit process［98］

Fig.23

Asynchronous emission process of cone-head and ellipsoid-head［107］

Fig.24

Three-dimensional trajectory curves of water⁃ exit process under different sea conditions［118］

Fig.25

Influence of brash ice on pressure of vehicle monitoring point during water-exit process［123］

Fig.26

Comparison of acceleration with different-sized holes of floating ice［127］

Fig.27

Comparison of pressure with different-sized holes of floating ice［127］

Fig.28

Holes in shoulders of ‘Polaris’ 4

Fig.29

Active ventilated cavitation technology of ‘M51’

Fig.30

Salvo launch of 4 vehicles