“…In addition, the turbulent heating rates calculated with two different turbulence models, including Baldwin-Lomax model and SST model, were observed to be in reasonable accordance in their studies. Wang et al [3] investigated the laminar and turbulent aeroheating performances of the MSL capsule with two distinct gas models, namely chemical non-equilibrium model and perfect gas model with specified effective specific heat ratio. Their studies revealed that laminar aeroheating calculated by the two gas models was nearly the same, whereas the turbulent heating rates predicted by chemical non-equilibrium model were much higher than perfect gas model at most areas of the heatshield.…”