Development of a mathematical model for the calculation of the "power weight" of aircraft structures based on the finite element method
Автор: Aliakbarov D.T., Rakhimkariev K.A.
Журнал: Теория и практика современной науки @modern-j
Рубрика: Основной раздел
Статья в выпуске: 6 (84), 2022 года.
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The paper is dedicated to solving the problem of determining the "power weight" of fuselage structures of prospective cargo aircraft using the finite element method. The order of calculation in solving static problems by the finite element method is given.
Cargo aircraft, finite element method, fuselage, power weight, mathematical model, stress-strain state
Короткий адрес: https://sciup.org/140294542
IDR: 140294542 | DOI: 10.46566/2412-9682_2022_84_52
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