Experimental Characterization of Aircraft Electromagnetic Protections

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Date
2021-12
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Advisor
Referee
Mark
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Volume Title
Publisher
Společnost pro radioelektronické inženýrství
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Abstract
In the paper, an original construction of a coaxial flange for measurements of shielding efficiency of composite materials is presented. The measurement procedure is conceived as a differential method to suppress influence of a flange. Attention is turned to measurements of carbon composites used in aerospace industry. The studied materials exhibit a significant ability to shield electromagnetic radiation. The shielding efficiency is rising with material thickness and with the number of fiber-to-fiber contacts. The optimal composite structure consists of 4 layers of carbon composite; more layers do not influence the shielding efficiency significantly.
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Citation
Radioengineering. 2021 vol. 30, č. 4, s. 654-661. ISSN 1210-2512
https://www.radioeng.cz/fulltexts/2021/21_04_0654_0661.pdf
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Peer-reviewed
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Language of document
en
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Defence
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Creative Commons Attribution 4.0 International license
http://creativecommons.org/licenses/by/4.0/
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