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Methodology for repeated load analysis of composite structures with embedded magnetic microwires

K. Semrád ; Faculty of Aeronautics, Technical University of Kosice, Slovakia
K. Draganová ; Faculty of Aeronautics, Technical University of Kosice, Slovakia

Puni tekst: engleski, pdf (256 KB) str. 175-178 preuzimanja: 275* citiraj
APA 6th Edition
Semrád, K. i Draganová, K. (2017). Methodology for repeated load analysis of composite structures with embedded magnetic microwires. Metalurgija, 56 (1-2), 175-178. Preuzeto s https://hrcak.srce.hr/168924
MLA 8th Edition
Semrád, K. i K. Draganová. "Methodology for repeated load analysis of composite structures with embedded magnetic microwires." Metalurgija, vol. 56, br. 1-2, 2017, str. 175-178. https://hrcak.srce.hr/168924. Citirano 28.01.2020.
Chicago 17th Edition
Semrád, K. i K. Draganová. "Methodology for repeated load analysis of composite structures with embedded magnetic microwires." Metalurgija 56, br. 1-2 (2017): 175-178. https://hrcak.srce.hr/168924
Harvard
Semrád, K., i Draganová, K. (2017). 'Methodology for repeated load analysis of composite structures with embedded magnetic microwires', Metalurgija, 56(1-2), str. 175-178. Preuzeto s: https://hrcak.srce.hr/168924 (Datum pristupa: 28.01.2020.)
Vancouver
Semrád K, Draganová K. Methodology for repeated load analysis of composite structures with embedded magnetic microwires. Metalurgija [Internet]. 2017 [pristupljeno 28.01.2020.];56(1-2):175-178. Dostupno na: https://hrcak.srce.hr/168924
IEEE
K. Semrád i K. Draganová, "Methodology for repeated load analysis of composite structures with embedded magnetic microwires", Metalurgija, vol.56, br. 1-2, str. 175-178, 2017. [Online]. Dostupno na: https://hrcak.srce.hr/168924. [Citirano: 28.01.2020.]

Sažetak
The article processes issue of strength of cyclically loaded composite structures with the possibility of contactless stress measuring inside a material. For this purpose a contactless tensile stress sensor using improved induction principle based on the magnetic microwires embedded in the composite structure has been developed. The methodology based on the E-N approach was applied for the analysis of the repeated load of the wing hinge connection, including finite element method (FEM) fatigue strength analysis. The results proved that composites in comparison with the metal structures offer significant weight reduction of the small aircraft construction, whereas the required strength, stability and lifetime of the components are remained.

Ključne riječi
fatigue strength analysis; magnetic microwires; composite structures; FEM

Hrčak ID: 168924

URI
https://hrcak.srce.hr/168924

Posjeta: 358 *