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Numerical Simulation of Planar Oscillations of a Landing Gear Leg along the Longitudinal Axis of an Aircraft During the Landing Impact. / Bagrov, K. V.

In: Journal of Applied and Industrial Mathematics, Vol. 13, No. 3, 01.07.2019, p. 385-389.

Research output: Contribution to journal › Article › peer-review

Harvard

Bagrov, KV 2019, 'Numerical Simulation of Planar Oscillations of a Landing Gear Leg along the Longitudinal Axis of an Aircraft During the Landing Impact', Journal of Applied and Industrial Mathematics, vol. 13, no. 3, pp. 385-389. https://doi.org/10.1134/S1990478919030013

APA

Bagrov, K. V. (2019). Numerical Simulation of Planar Oscillations of a Landing Gear Leg along the Longitudinal Axis of an Aircraft During the Landing Impact. Journal of Applied and Industrial Mathematics, 13(3), 385-389. https://doi.org/10.1134/S1990478919030013

Vancouver

Bagrov KV. Numerical Simulation of Planar Oscillations of a Landing Gear Leg along the Longitudinal Axis of an Aircraft During the Landing Impact. Journal of Applied and Industrial Mathematics. 2019 Jul 1;13(3):385-389. doi: 10.1134/S1990478919030013

Author

Bagrov, K. V. / Numerical Simulation of Planar Oscillations of a Landing Gear Leg along the Longitudinal Axis of an Aircraft During the Landing Impact. In: Journal of Applied and Industrial Mathematics. 2019 ; Vol. 13, No. 3. pp. 385-389.

BibTeX

@article{117a5dabe8ed4594b15f9fbdb77120e7,
title = "Numerical Simulation of Planar Oscillations of a Landing Gear Leg along the Longitudinal Axis of an Aircraft During the Landing Impact",
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 = "gear-walk deformation, landing gear, nonlinear damping, oleo strut",
author = "Bagrov, {K. V.}",
year = "2019",
month = jul,
day = "1",
doi = "10.1134/S1990478919030013",
language = "English",
volume = "13",
pages = "385--389",
journal = "Journal of Applied and Industrial Mathematics",
issn = "1990-4789",
publisher = "Maik Nauka-Interperiodica Publishing",
number = "3",

}

RIS

TY - JOUR

T1 - Numerical Simulation of Planar Oscillations of a Landing Gear Leg along the Longitudinal Axis of an Aircraft During the Landing Impact

AU - Bagrov, K. V.

PY - 2019/7/1

Y1 - 2019/7/1

N2 - 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.

AB - 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.

KW - gear-walk deformation

KW - landing gear

KW - nonlinear damping

KW - oleo strut

UR - http://www.scopus.com/inward/record.url?scp=85071507811&partnerID=8YFLogxK

U2 - 10.1134/S1990478919030013

DO - 10.1134/S1990478919030013

M3 - Article

AN - SCOPUS:85071507811

VL - 13

SP - 385

EP - 389

JO - Journal of Applied and Industrial Mathematics

JF - Journal of Applied and Industrial Mathematics

SN - 1990-4789

IS - 3

ER -

ID: 21472242