Figure 16. Distributions of Mach number at the inlet of nozzle 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