Figure 12. Distribution of stagnation pressure on the axis of symmetry (through the wind tunnel from nozzle’s inlet to diffuser’s outlet) for three different turbulence models of SST/k-ω, RNG/k-ε and Realizable/k-ε

From

Analysis of Different Turbulence Models in Simulation of Hypersonic Flow in the Wind Tunnel

Mohammad Javad Ameri, Mohammad Reza Heidari, Hashem Nowruzi, Amin Najafi

American Journal of Mechanical Engineering. 2019, 7(4), 172-180 doi:10.12691/ajme-7-4-3