Experimental Characterization of Aircraft Electromagnetic Protections
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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.
KeywordsCarbon composite, carbon-fiber-reinforced polymer (CFRP), glass-fiber composite (GFC), shielding efficiency, measurements, aerospace applications, coaxial flange
Document typePeer reviewed
Document versionFinal PDF
SourceRadioengineering. 2021 vol. 30, č. 4, s. 654-661. ISSN 1210-2512
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