Table 1

Inflow conditions of flat plate

Fig.1

Comparison of Van Driest average velocity profile at velocity thickness δ=0.007 7 m

Fig.2

Skin friction coefficient over flat plate

Fig.3

Pressure and temperature profile in turbulent boundary layer at δ=0.007 7 m

Table 2

Inflow conditions of Ma∞ =2.9 ramp

Fig.4

Structural grid of 24° compression ramp

Fig.5

Wall pressure distribution of 24° compression ramp

Fig.6

Eddy viscosity contours superimposed density gradient isolines of 24° compression ramp

Fig.7

Temperature contours superimposed Fs isolines of 24° compression ramp

Fig.8

Streamline and eddy viscosity isoline of 24° compression ramp

Fig.9

Comparison of eddy viscosity distribution at y=10-5 m on central slice of 24° compression corner

Table 3

Supersonic inflow conditions of isolator［43-45］

Fig.10

Schematic diagram of computational isolator

Fig.11

Wall pressure profile of central slice in pipe

Fig.12

Flow velocity contours near symmetry plane and wall surface

Fig.13

Eddy viscosity contours， eddy viscosity isoline and streamline near symmetry plane and wall surface

Fig.14

Turbulent kinetic energy contours and Ma=1 isoline of central slice in pipe

Fig.15

HIFiRE-2 combustion chamber calculation domain and grid distribution

Table 4

Supersonic flow conditions of HIFiRE⁃2 internal channel

Fig.16

Comparison of calculation results and test values of wall pressure in HIFiRE-2 internal channel

Fig.17

Flow velocity contours （right） and normalized turbulent kinetic energy contours （left） superimposed normalized turbulent kinetic energy and shock discriminant function Fs isoline

Fig.18

Eddy viscosity contours and eddy viscosity isoline of flow field superimposed streamline and Ma=1 isoline