DETERMINATION OF MECHANICAL CHARACTERISTICS OF AIRCRAFT WING PANELS

Authors

DOI:

https://doi.org/10.30888/2709-2267.2024-23-00-013

Keywords:

Composite materials, monolayer, carbon tape, carbon fabric

Abstract

The paper presents the method of calculating the mechanical characteristics of multilayer composite panels. The optimal sequence of laying out monolayers was selected. The mechanical behavior of the composition is determined by the ratio of the properties

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References

Klyuchnikov Yu. V., Serditov O. T., Dubnyuk V. L. Aviacijni materiali ta yih tehnologiyi: navch. posibnik / Nacionalnij tehnichnij universitet Ukrayini «Kiyivskij politehnichnij institut imeni Igorya Sikorskogo», Kiyiv,2022. – 114s.

Zhao Qun, Ding Yunliang, Jin Haibo. A Layout Optimization Method of Composite Wing Structures Based on Carrying Efficiency Criterion // Chinese Journal of Aeronautics. –No24, 2017. –P. 425

Vasilevskij E.T. Sistema eksperimentalnogo obespecheniya rascheta na prochnost mehanicheskih soedinenij detalejiz kompozitov / E.T. Vasilevskij, A.Z. Dvejrin, Ya.S. Karpov, S.P. Krivenda // Otkrytye informacionnye i kompyuternye integrirovannye tehnologii. – H.: NAKU “HAI”, 2010. – № 47. – S. 42 – 52.

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Published

2024-03-30

How to Cite

Alekseychuk, O., & Trubachev, S. (2024). DETERMINATION OF MECHANICAL CHARACTERISTICS OF AIRCRAFT WING PANELS. Sworld-Us Conference Proceedings, 1(usc23-01), 11–15. https://doi.org/10.30888/2709-2267.2024-23-00-013

Issue

No. usc23-01 (2024): Organization of scientific research in modern conditions '2024

Section

Abstracts

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