Articles you may be interested inTrajectory optimization study of a lifting body re-entry vehicle for medium to intermediate range applications AIP Conf. Proc. 1493, 782 (2012); 10.1063/1.4765577 Model surface conductivity effect for the electromagnetic heat shield in re-entry flight Phys. Fluids 20, 127103 (2008); 10.1063/1.3054149 MHD waves in stratified and dissipative plasmas AIP Conf.Abstract: In the present work, starting from classical MHD scheme, based on Maxwell equations, Euler fluid dynamic equations and generalised Ohm law, a critical study of fluid dynamics, electromagnetism, chemical and physical behaviour of plasma is carried out, and then a aircraft re-entry MHD numerical scheme is implemented. This scheme is used for MHD calculations in different conditions, in the range of low magnetic force and intermediate electrical conductivity. Initial imposed magnetic fields are uniform, but also some cases with coil generated magnetic fields are considered. Calculations of magnetic field and induced currents are extended also inside the blunt body. Results show interesting physical and electromagnetic effects. Comparison with other methods shows possible development in keeping into account other physical and chemical effects.