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access icon openaccess Simulation and analysis of EMP transient electromagnetic effect of aircraft

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References

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      • 1. Wen, H., Hou, X., Wang, H.: ‘Experimental study on lightning attachment point of aircraft model’, High Volt. Technol., 2006, 32, (7), pp. 9092.
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      • 2. Teng, X., Liu, G., Yu, Z., et al: ‘Study on division of aircraft lightning attachment area’, Microw. Sin., 2014, 30, (4), pp. 1419.
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      • 3. Duan, Z., Cao, K., Cheng, Z.: ‘Test and waveform of aircraft lightning protection’, High Volt. Technol., 2000, 26, (4), pp. 6163.
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      • 4. Luo, L.: ‘Lightning indirect effect test and analysis of the standard [J]’, Electron. Sci. Technol., 2014, 1, (1), pp. 97100.
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      • 5. Perrin, E., Guiffaut, C., ReineixL, A.: ‘Using a design-of-experiment technique to consider the wire harness load impedances in the FDTD model of an aircraft struck by lightning’, IEEE Trans. Electromagn. Compat., 2013, 55, (4), pp. 747752.
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      • 6. Huang, L., Gao, C., Guo, F.: ‘Lightning indirect effects on helicopter: numerical simulation and experiment validation’, IEEE Trans. Electromagn. Compat., 2017, 59, (4), pp. 11711179.
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      • 7. Gaynutdinov, R.R., Chermoshentsev, S.F.: ‘Study of lightning strike impact on unmanned aerial vehicle’. 2016 17th Int. Conf. of Young Specialists on Micro/Nanotechnologies and Electron Devices (EDM), Erlagol, Russia, 2016.
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