Abstract
The paper deals with the analytical solution of the problem on the laminar hydrodynamic thermal boundary layer with internal heat release, formed in a flat channel with a nonuniform wall temperature under conditions of steady-state flow of compressible gas irradiated by fission fragments. Subsonic velocities of pumping flow are treated, which are much lower than the velocity of sound.
Published Version
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have