Numerical continuation analysis of a three-dimensional aircraft main landing gear mechanism

A method of investigating quasi-static landing gear mechanisms is presented and applied to a three-dimensional aircraft main landing gear mechanism model. The model has 19 static equilibrium equations and 20 equations describing the geometric constraints in the mechanism. In the spirit of bifurcatio...

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Bibliographic Details

Main Authors:	James Knowles, Bernd Krauskopf, Mark H. Lowenberg
Format:	Default Article
Published:	2013
Subjects:	Other engineering not elsewhere classified Landing gear Bifurcation analysis Numerical continuation Engineering not elsewhere classified
Online Access:	https://hdl.handle.net/2134/15941
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