*Aero Heating Optimization of a Hypersonic Thermochemical Non-Equilibrium Flow… DOI: http://dx.doi.org/10.5772/intechopen.101659*

and free stream flow, induces a redistribution of the temperature in the mixing zone ward off the normal shock from the nose blunt body about 0.3 mm, which allows the reduction of the wall heat transfer of the body by approximately 28.75%, this cooling system must be associated with important subsystems, particularly in terms of feasibility constrained by the mass and layout problems (regulator, pump, storage tank of gaze, etc.).
