The invention provides gun,
artillery and
rocket jet engines, steam turbines, internal
combustion engines and air vehicles with an additional magnetic device. A
magnet is included,
translational motion, through
Lorentz force, rotation and vibration of fluid molecules near the
magnet in the direction of being perpendicular to the micro-flow direction of fluid are strongly inhibited, and pressure and temperature of the fluid molecules in the direction of being perpendicular to the micro-flow direction of the fluid are significantly lowered, so that the speed that the fluid molecules diffuse in the needed micro-flow direction is significantly increased.
Viscous friction, turbulent
shear stress,
friction force and heat conduction in a boundary layer and shock
waves, resistance generated by the shock
waves and negative influences of heating on relative movement between air flow and an object are eliminated fundamentally in the microcosmic level or at least weakened greatly. By equipping the
magnet on various gun,
artillery and
rocket engines, jet engines, turbines,
gasoline engines, diesel engines and the like,
radial pressure and temperature must be significantly lowered, the initial speed of pills is significantly increased, the power and the speed of the rock engines and the jet engines are increased, the energy
utilization rate of the
gas turbines, the turbines and the internal
combustion engines is increased, and various resistances borne by the air vehicles and heating of the air vehicles are significantly reduced.