Numerical Study Of The Compressible Flow Inside A Supersonic Nozzle To 2D
The object of this study is performed phenomena, which appear in the flow of a two-dimensional convergentdivergent
nozzle. The fluid used is a gas, which assumed to be an ideal gas, by using the finite volume method for solving
partial differential equations and turbulence model used in this study is the model with two types of transport equations (k-ω)
SST Menter, is considered the most suitable for this kind of problem. This simulation performed using FLUENT software.
Keywords—nozzle, converging-diverging, turbulence, shock wave, supersonic, compressible flow, finite volume.