Influence of Variable Side-Stay Geometry on the Shimmy Dynamics of an Aircraft Dual-Wheel Main Landing Gear-Reference-Cited by-同舟云学术

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Influence of Variable Side-Stay Geometry on the Shimmy Dynamics of an Aircraft Dual-Wheel Main Landing Gear

Published:2013-01 Issue:3 Volume:12 Page:1181-1209
ISSN:1536-0040
Container-title:SIAM Journal on Applied Dynamical Systems
language:en
Short-container-title:SIAM J. Appl. Dyn. Syst.

Author:

Howcroft Chris,Krauskopf Bernd,Lowenberg Mark H.,Neild Simon A.

Publisher

Society for Industrial & Applied Mathematics (SIAM)

Subject

Modeling and Simulation,Analysis

Link

http://epubs.siam.org/doi/pdf/10.1137/120887643

Reference38 articles.

1. Bifurcation Analysis of Nonlinear Aircraft Dynamics

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1. Distribution of the residual tolerable imbalance between correction plans;Mechanics Based Design of Structures and Machines;2024-06-22

2. An Updating Method of Aero Tyre Model by Shimmy Test;Lecture Notes in Mechanical Engineering;2023-12-20

3. Parameter effects on high-speed UAV ground directional stability using bifurcation analysis;Chinese Journal of Aeronautics;2021-11

4. Unlocking a nose landing gear in different flight conditions: folds, cusps and a swallowtail;Nonlinear Dynamics;2021-10-12

5. Sensitivity Analysis for the Shimmy Dynamics of an Airplane Main Landing Gear;Journal of Applied Nonlinear Dynamics;2021-10-01

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