Research Article

Investigation of the Effects of Length to Depth Ratio on Open Supersonic Cavities Using CFD and Proper Orthogonal Decomposition

Table 1

Numerical and experimental parameters for the preliminary CFD study.

Total pressure66.4 kPa
Total temperature218 K
Mach number1.5
Reynolds number
Cavity length0.12065 m
Cavity depth0.0238 m
Boundary layer thickness0.0051 m