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This article is cited in 4 scientific papers (total in 4 papers)
Numerical simulation of planar oscillations of a landing gear leg along the longitudinal axis of an aircraft during the landing impact
K. V. Bagrov Novosibirsk State University,
ul. Pirogova 1,
630090 Novosibirsk
Abstract:
The study is presented of the aircraft landing gear deformations in the axial direction of the aircraft (gear-walk) under the load from a runway. Some beam-based model is proposed to describe the elastic properties of landing gear and the oleo strut behavior. The primary verification of the model is carried out: The characteristic frequencies of oscillations are found, and the behavior of the system under harmonic load is investigated.
Keywords:
oleo strut, landing gear, nonlinear damping, gear-walk deformation.
Received: 14.06.2018 Revised: 14.06.2018 Accepted: 14.03.2019
Citation:
K. V. Bagrov, “Numerical simulation of planar oscillations of a landing gear leg along the longitudinal axis of an aircraft during the landing impact”, Sib. Zh. Ind. Mat., 22:3 (2019), 3–7; J. Appl. Industr. Math., 13:3 (2019), 385–389
Linking options:
https://www.mathnet.ru/eng/sjim1049 https://www.mathnet.ru/eng/sjim/v22/i3/p3
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Abstract page: | 253 | Full-text PDF : | 65 | References: | 39 | First page: | 7 |
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