Finite-rate chemistry in hypersonic shock-wave/turbulent boundary-layer interaction produces a smaller separation bubble, lower wall heat flux, and lower temperatures than perfect-gas models at Me=6.4 and He=16.9 MJ/kg.
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Effects of thermochemical modelling on a hypersonic shock-wave/turbulent boundary-layer interaction
Finite-rate chemistry in hypersonic shock-wave/turbulent boundary-layer interaction produces a smaller separation bubble, lower wall heat flux, and lower temperatures than perfect-gas models at Me=6.4 and He=16.9 MJ/kg.