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

DOI10.1137/120887643zbMath1282.70044OpenAlexW2039834651MaRDI QIDQ2871361

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

Publication date: 22 January 2014

Published in: SIAM Journal on Applied Dynamical Systems (Search for Journal in Brave)

Full work available at URL: https://research-information.bris.ac.uk/ws/files/34722841/Howcroft_et_al_2013.pdf

zbMATH Keywords

bifurcation analysisshimmy oscillationsaircraft ground dynamicsmain landing gear model

Mathematics Subject Classification ID

Bifurcations and instability for nonlinear problems in mechanics (70K50) Nonlinear oscillations and coupled oscillators for ordinary differential equations (34C15) Nonlinear resonances for nonlinear problems in mechanics (70K30)

Related Items (3)

Numerical continuation and bifurcation analysis in aircraft design: an industrial perspective ⋮ Unlocking a nose landing gear in different flight conditions: folds, cusps and a swallowtail ⋮ Nonlinear energy sink to enhance the landing gear shimmy performance

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