Numerical Simulation of Planar Oscillations of a Landing Gear Leg along the Longitudinal Axis of an Aircraft During the Landing Impact

Результат исследования: Научные публикации в периодических изданияхстатья

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 оригиналаанглийский
Страницы (с-по)385-389
Число страниц5
ЖурналJournal of Applied and Industrial Mathematics
Том13
Номер выпуска3
DOI
СостояниеОпубликовано - 1 июл 2019

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