Figure 8. Static pressure distribution around the HB-2 : (a) measured at HST2 [27] and (b) present study under the Mach number 8 and Mach number distribution around the HB-2 : (c) measured at HST2 [27] and (d) present study

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