The paper deals with two-dimensional mathematical models of radiation-
gasdynamic processes in Laval nozzles of laser-plasma accelerators. On
e of the models is based on the solution of Navier-Stokes equations fo
r subsonic compressible flows in the ''velocity-pressure'' variables.
The other model involves the use of dynamic variables. The finite-diff
erence schemes are constructed on the basis of equations written in th
e conservative form in nonorthogonal coordinates. The results are pres
ented of calculations of the thermogasdynamic structure of atmospheric
-pressure air flows under conditions of their local heating by focused
radiation of a continuous CO2 laser. Analysis is made of radiation-ga
sdynamic processes for different values of laser power, flow velocity,
and nozzle size.