Method for acquiring electric field distribution of large-sized complex aircraft by using fast boundary element method
A technology of boundary element method and electric field distribution, which is applied in the direction of instruments, electrical digital data processing, special data processing applications, etc., can solve problems such as complex singular integral processing, broken boundary continuity, difficult high precision, etc.
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[0059] Now in conjunction with embodiment, accompanying drawing, the present invention will be further described:
[0060] Taking the capacitance calculation problem of an aircraft model as an example, it is implemented according to the technical solution of the present invention, and a detailed implementation process is given.
[0061] To calculate the capacitance of an aircraft model, the core is to solve the boundary integral equation on the boundary S of the aircraft
[0062] ∫ S K(x,y)σ(y)dy=f(x)
[0063] where K(x,y)=1 / (4πε 0 |x-y|), ε 0 =8.8541878 is the vacuum permittivity, f(x) is a known function, and σ(y) is a function to be found. The main steps of applying the fast numerical method for aircraft electric field analysis are as follows:
[0064] 1. Build a geometric model. CAD software (such as Pro-E, etc.) can be used to establish the aircraft boundary surface model according to the actual size, and save it in IGES format, which contains the parameter equation...
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