Influence of Thermochemical Nonequilibrium on Characteristics of Boundary Layer at Flight in the Martian Atmosphere

In framework on the eN-method, comparative calculations of position beginning zone of laminar-turbulent transition completed for two points on landing trajectory of “Pathfinder” spacecraft on surface of the Mars. The calculations used a three-component model of a thermochemical nonequilibrium mixture CO2=CO=O. The set of frequencies of spatial disturbances is determined along neutral curves for first unstable modes of temporary disturbances. The transition Reynolds number Re T was determined from envelopes of families of the N-factor curves at NT=8. In hypersonic regime at M=12:6, taking into account the developed thermochemical nonequilibrium leads to a significant decrease in the static temperature of gas in the lower part of the boundary layer. As a result, beginning of the zone of laminar-turbulent transition shifts downstream by approximately 9% compared to case of a perfect gas.