Fig.1

Throttling characteristics of four-lip supersonic Bump inlet

Fig.2

Throttling characteristics of a 2-D supersonic inlet

Fig.3

Throttling characteristics of a supersonic Caret inlet

Fig.4

Throttling characteristics of a supersonic Bump inlet

Fig.5

Low energy zone on bump surface of Bump inlet at design state

Fig.6

Spillage low energy air on bump surface at design state

Fig.7

Surface shear stress lines of Bump inlet at design state

Fig.8

Separation bubbles and separation shock on symmetry plane of Bump inlet

Fig.9

Separation bubbles deviating from symmetry plane of Bump inlet

Fig.10

Low total pressure recovery zone on Bump inlet at low mass flow state

Fig.11

Low energy air on bump surface of inlet at low mass flow state

Fig.13

Surface shear stress lines of Bump inlet at low mass flow state

Fig.14

Wind tunnel experimental model with/without boundary layer suction on bump surface of Bump inlet

Fig.15

Bump inlet aerodynamic performance with/without boundary layer suction

Fig.16

Wedge compression and Bump compression inlet with same forward swept cowl

Fig.17

Surface shear stress lines on wedge compression inlet at design state

Fig.18

Separated flow of wedge compression inlet at design state

Fig.19

Throttling characteristics of wedge compression and Bump compression inlet with same forward swept cover

Fig.20

Buzz induced by separated flow in wedge compression inlet at low mass flow state

Fig.21

Surface shear stress lines of wedge compression inlet at low mass flow state

Fig.22

Surface shear stress lines on cone compression inlet at design state

Fig.23

Surface shear stress lines on cone compression inlet at subcritical state