Disclosed are a method for designing
lightning shielding by using diverter strips on an aircraft, a
system, a device, and a medium. The method comprises: determining boundary conditions of a
simulation space; according to the boundary conditions of the
simulation space, performing numerical calculation on an
electric field in the
simulation space; according to the calculation result of the
electric field and in combination with fractal theory, determining a probability of the direction of
lightning leader development, and, according to the probability of the direction of
lightning leader development, randomly selecting a subsequent development position of a lightning downward-moving stepped leader; determining, on the basis of testing and simulation results of a
corona discharge characteristic at the tip of a
metal electrode having a small
radius of curvature, whether an initial
corona at an end portion of a diverter strip has been initiated, and determining whether an initial
corona at an end portion of a diverter strip has been initiated; determining whether the lightning downward-moving stepped leader can, after attaching to an insulating plate, run through a gap along the surface and reach an adjacent diverter strip; repeating the process above, and performing multiple simulations to solve the probability of lightning protection of diverter strips and establish a relationship between the probability of lightning protection of diverter strips and the distance between the diverter strips at different thicknesses of and using different materials for the insulating plate.