Figure 13. Distribution of static pressure at the inlet of the test chamber 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