Numerkal methods application for estimation shoc-wave interaction with thermal layer

The shock-wave interaction with thermal layer over hard flat surface is studied with the help of Navier–Stokes equations for heat compressed gas. For accuracy control the estimation is carried out with explicit and implicit difference scheme. Intensity of shock-wave, temperature of thermal layer and geometric property: thermal layer thickness, distance from surface, height of explosio is varying in the numerical experiments. Essential influence of these parameters on the flow structure is established.