“…The thermal plasma/gas regions are always present, for example, in the energy deposition experiments and they are described, in the absence of diffusion, as nonuniform gas objects, with a temperature profile for the initial temperature distribution that can be approximated with a Gaussian function. 23 The effects of the shock-plasma interaction have been an area of interest mostly due to its applications in aerospace for aerodynamic flow control in supersonic flights and for atmospheric reentry; 14,[24][25][26][27][28][29][30][31][32][33][34][35] in MHD for shock wave structure control; in astrophysics for shock waves generated in stellar interior; 15,16 and in environmental science for sonic boom suppression. Another area of considerable interest is the shock wave assisted combustion, where a shock wave can be used to affect the ignition conditions in the gas.…”