Coupled heat transfer between a viscous shock gasdynamic layer and a transversely streamlined anisotropic half-space

Abstract

The purpose of the article is to analytically solve the conjugate problem of heat transfer in a viscous shock layer on a blunt object and thermal conductivity in an anisotropic half-space. A feature of the flow around such bodies near the critical point is that in this case, the boundary layer equations are not satisfied and it is necessary to solve the Navier-Stokes equations together with the equations of continuity, state, and energy, however, in a stationary formulation of an incompressible flow. The problem of coupled heat transfer between a viscous shock gasdynamic layer and anisotropic half-space with the assumption of incompressibility of the gasdynamic flow behind the normal part of the shock wave is posed. An analytical solution to this problem is obtained with a boundary condition at the gas-solid object interface in the form of a parameter – temperature, as well as an analytical solution to the thermal conductivity problem in an anisotropic half-space with the same boundary condition.

Conductive Heat Transfer in Materials under Intense Heat Flows

“…Classical theories of heat conduction as applied to solving various complex problems of mechanics were used in [9][10][11][12].…”

Effect of High Velocity Deformation on Strength of ArmoredComposite Materials

“…During loading, a material subjected to high-rate deformation may change its mechanical properties, in comparison with the properties found as a result of static tests [1][2][3][4][5][6][7][8]. To calculate the structures under consideration, it is necessary to assess the effect of the strain rate on the properties of the materials used [9][10][11][12][13][14][15][16]. Therefore, the high-speed properties of CFRP were investigated, from which the master device of the product can be made.…”