Numerical Investigation on the Effect of Inflow Mach Numbers on the Combustion Characteristics of a Typical Cavity-Based Supersonic Combustor

Figure 5

Comparison of the experimental and simulation velocity profiles at streamwise locations (a) 125 mm and (b) 207 mm. Comparison of the experimental (c) shadow image with the contours of the (d) density and (e) pressure.

(a)

(b)

(c)

(d)

(e)