2SAE. ARP5412 Aircraft Lightning Environment andRelated Test Waveforms[S]. Warrendale,PA: Socie-ty of Automotive Engineers, 1999. 被引量：1
3SAE. ARP5414 Aircraft Lightning Zoning[S]. War-rendale, PA: Society of Automotive Engineers? 2005. 被引量：1
4SAE. ARP5416 Aircraft Lightning Test Methods[S].Warrendale PA: Society of Automotive Engineers,2005. 被引量：1
5USDOD. MIL-STD-464, Electromagnetic Environ-ment Effects Requirements for Systems[S], U. S. A :United States Department of Defense,1997. 被引量：1
6USDOD. MIL-STD-1757, Lightning QualificationTest Techniques for Aerospace Vehicles and Hard-ware[S]. U. S. A: United States Department of De-fense ,1980. 被引量：1
7USDOD. MIL-STD-1795, Lightning Protection ofAerospace Vehicles and Hardware [S]. U. S. A; U-nited States Department of Defense, 1989. 被引量：1
8PERALA R A,RUDOLPH T H,MCKENNA P M,et al. Application of numerical analysis to the electro-magnetic effects validation of aircraft[C]// 12th Digit-al Avionics Systems Conference. Fort Worth, October25-28, 1993: 185-190. 被引量：1
9PERALA R A, ELLIOT J R,CURRY J D. Theeffects of simulated electromagnetic pulse on commer-cial aircraft [J ]. IEEE Trans Electromagnetic Com-patibility, 1991,33(2) : 120-131. 被引量：1
10MAURIZIO A,MARCELLO D. Lightning indirecteffects certification of a transport aircraft by numericalsimulation [J]. IEEE Trans Electromagnetic Compat-ibility, 2008, 50(3): 513-523. 被引量：1
