A simplified one-dimensional model was proposed to treat the gas dynam
ic problems in a supersonic jet, which was used to produce radicals co
oled by supersonic expansion. Based on this model, the gas dynamic equ
ations can be integrated directly to obtain the evolution of the trans
lational temperature and the rotational temperature of free radicals a
s well as the molecule density. The results show that the heating posi
tion where the radicals are generated and the initial rotational tempe
rature of radicals have little effect on the rotational temperature at
the down stream detection point, if the heating position is close to
the nozzle orifice.