Numerical Calculation of the Stress-Strain State of an Aircraft Nacelle Attachment Element
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Дата
2025-03-08
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Видавець
Cognum Publishing House
Анотація
This paper presents the results of numerical modeling of the stress-strain state of the strut of a transport aircraft nacelle using the finite element method (FEM). The objective is to construct a computational model and analyze the stress-strain state (SSS) of the nacelle attachment element under combined loads occurring during aircraft operation.
Опис
Ключові слова
Stress-strain state, finite element method, nacelle, numerical modeling, strut
Бібліографічний опис
Pyskunov, S. O. Numerical Calculation of the Stress-Strain State of an Aircraft Nacelle Attachment Element / Pyskunov S. O., Trubachev S. I., Prykhodko M. V. // Scientific achievements of contemporary society : Proceedings of VIII International Scientific and Practical Conference, [London, United Kingdom], 6-8 March 2025. - London, 2025. - Pp. 151-154.