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Fig
ure
15
.
Distribution of static pressure 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
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