State-to-state catalytic models, kinetics, and transport in hypersonic boundary layers

A new iterative model has been developed that couples, in the boundary layer of a reentering body, the equations for N-2, N, O-2, O, and NO mass fractions, N-2 and O-2 Vibrational distributions, and gas temperature with the surface state-to-state heterogeneous recombination coefficients has been developed. Results for SiO2 and metallic surfaces are presented and discussed. The non-Boltzmann behavior of the vibrational distribution functions near the surface is found, as well as the nonmonotonic behavior of the NO density profile along the boundary layer coordinate. The transport coefficients and the heat flux to the surface are calculated using the Chapman-Enskog theory. A strong dependence of transport coefficients and energy flux on the vibrational-chemical kinetics in the boundary layer is shown. In particular, the diffusion coefficients of the first and last vibrational levels differ by several orders of magnitude, according to the shape of vibrational distributions, and the surface material noticeably influences diffusion coefficients of N and NO.