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contributor authorMcHugh, Kevin A.
contributor authorDowell, Earl H.
date accessioned2022-02-04T22:58:34Z
date available2022-02-04T22:58:34Z
date copyright2/1/2020 12:00:00 AM
date issued2020
identifier issn1555-1415
identifier othercnd_015_02_021003.pdf
identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4275822
description abstractA free–free beam with a compressive follower force applied to one end exhibits interesting flutter and limit cycle oscillation (LCO) responses. Here, the derivation from Lagrange's equations is given for the nonlinear inextensible beam with such a force applied. The inextensibility constraint is met with a Lagrange multiplier added to the Lagrangian, and the beam allowed three rigid body modes in planar motion in addition to its elastic deformation. The Rayleigh–Ritz modal expansion method and the Runge–Kutta method are used to calculate time histories of the forced beam response. This new model is validated against classical results for the stability boundary and new LCO bifurcation diagrams are computed.
publisherThe American Society of Mechanical Engineers (ASME)
titleNonlinear Response of an Inextensible, Free–Free Beam Subjected to a Nonconservative Follower Force
typeJournal Paper
journal volume15
journal issue2
journal titleJournal of Computational and Nonlinear Dynamics
identifier doi10.1115/1.4045532
journal fristpage021003-1
journal lastpage021003-12
page12
treeJournal of Computational and Nonlinear Dynamics:;2020:;volume( 015 ):;issue: 002
contenttypeFulltext


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