Published October 2008 | Version v1
Journal article

Stability analyses for axially moving strings in nonlinear free and aerodynamically excited vibrations

  • 1. Department of Engineering Mechanics, Dalian University of Technology, 2 Linggong Road, Dalian 116024 (China)
  • 2. State Key Laboratory of Structural Analysis for Industrial Equipment, Dalian University of Technology, Dalian 116024 (China)
  • 3. School of Civil Engineering and Hydraulic Engineering, Dalian University of Technology, 2 Linggong Road, Dalian 116024 (China)

Description

Nonlinear free vibration and stability problems are investigated for axially moving strings in transverse motions. The equation of nonlinear, free motion is derived and discretized using the Galerkin's method. The method of multiple time scale is adopted to obtain the approximate response. It is pointed out that the motion stays stable for transportations with speed less than the linear critical speed. For taut strings that move with large transport speeds, the stability of the equilibrium configuration under steady aerodynamic excitation is explicitly analyzed. Based on the Routh-Hurwitz criterion, the condition for Hopf bifurcation is presented with multiple parameters for transverse motions perturbed in the vicinity of the equilibrium configurations

Availability note (English)

Available from http://dx.doi.org/10.1016/j.chaos.2006.11.017

Additional details

Identifiers

DOI
10.1016/j.chaos.2006.11.017;
PII
S0960-0779(06)01059-9;

Publishing Information

Journal Title
Chaos, Solitons and Fractals
Journal Volume
38
Journal Issue
2
Journal Page Range
p. 421-429
ISSN
0960-0779

INIS

Country of Publication
United Kingdom
Country of Input or Organization
International Atomic Energy Agency (IAEA)
INIS RN
40012799
Subject category
S71: CLASSICAL AND QUANTUM MECHANICS, GENERAL PHYSICS;
Descriptors DEI
BIFURCATION; EQUATIONS; EQUILIBRIUM; EXCITATION; GALERKIN-PETROV METHOD; NONLINEAR PROBLEMS; STABILITY
Descriptors DEC
CALCULATION METHODS; ENERGY-LEVEL TRANSITIONS; ITERATIVE METHODS

Optional Information

Copyright
Copyright (c) 2006 Elsevier Science B.V., Amsterdam, The Netherlands, All rights reserved.