Аннотация
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.
Язык оригинала | английский |
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Страницы (с-по) | 385-389 |
Число страниц | 5 |
Журнал | Journal of Applied and Industrial Mathematics |
Том | 13 |
Номер выпуска | 3 |
DOI | |
Состояние | Опубликовано - 1 июл 2019 |