The modeling of a supersonic air nozzle flow is presented and compared with
measurements at the nozzle exit. Shortcomings of state-of-the-art models f
or the kinetic scheme and energy exchange terms are discussed. In particula
r, the significant influence of an accurate modeling of vibrational-transla
tional and vibrational-vibrational energy exchanges is shown. Conversely, t
he choice of the model for the kinetic scheme and for the chemical-vibratio
nal energy exchange term only has a small influence on the results.