Figure 21. Flow streamlines at the diffuser for (a) RNG/k-ε, (b) Realizable/k-ε and (c) SST/k-ω

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