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

Figure 3

(a) Comparisons of the Schlieren images and flame luminosity images with the density and temperature contours obtained from the simulations. (b) Static wall distribution along the upper wall of the cavities and comparing the experimental and simulation work with the present simulations.

(a)

(b)