flow structure of the interaction shows but clearly defined complex shock seen to underexpanded and 147plumes148 into a barrel with the terminal shock resulting into a supersonic been observed T ID: 849415
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1 Supersonic Freestreams with Counterflowi
Supersonic Freestreams with Counterflowing Mail Code Flight Center, Flight Center Marshall Space Flight Center flow structure of the interaction shows but clearly defined complex shock seen to underexpanded and “plumes” into a barrel with the terminal shock resulting into a supersonic been observed The shock seen to mass flow rate is increased, thus indicating a weaker reduction in However, for the observed in heat is different from the cooling of the in the heat
2 data shows that expanded, the some criti
data shows that expanded, the some critical trend of the heat flux flow rate is the same outer rows flux gauges. shock standoff given below. The broken section of the represent the the shock can not classical sense since the shocks the conventional supersonic and hypersonic flows such as into and re-entry atmospheres, the observed interactions and structures could harsh aerothermal environments and aerodynamic performance. of heat flux In fact the data heat flux, that the fl
3 ow in the heat shield was having a effec
ow in the heat shield was having a effect instead the shock induced heating that model would experienced. Such could have a traditional thermal to significantly reduce the with the environment at into planetary addition to other potential and free be used above are experimental results of supersonic flowfields with counterflowing The complete data, including videos and the benefits of the ccounterflowing of planetary will be full paper. atmospheric entry and Scale Apollo Mod