2014
DOI: 10.1051/matecconf/20141603006
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Nonlinear responses of externally excited rotor bearing system

Abstract: Abstract. A mathematical model incorporating higher order deformation in bending is developed to investigate the nonlinear behavior of rotor. Transverse harmonic base excitation is imparted to rotor system and Euler-Bernoulli beam theorem is applied with effects such as rotary inertia, gyroscopic effect, higher order large deformations, rotor mass unbalance and dynamic axial force. Discretization of the kinetic and strain (deformation) energies of the rotor system is done using the Rayleigh-Ritz method. Second… Show more

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Cited by 2 publications
(5 citation statements)
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“…Setting the discriminant of eqn. (25) to zero, the expression for determining the critical values of đť‘Ž 1 is obtained as…”
Section: Critical Parameter Values For the Emergence Of Jump Phenomen...mentioning
confidence: 99%
See 3 more Smart Citations
“…Setting the discriminant of eqn. (25) to zero, the expression for determining the critical values of đť‘Ž 1 is obtained as…”
Section: Critical Parameter Values For the Emergence Of Jump Phenomen...mentioning
confidence: 99%
“…Only the literatures on the modelling and analyses of non-linear rotor system are discussed in this part. The rotor system models can be broadly categorized into: (i) discrete [1-16] and (ii) continuous [17][18][19][20][21][22][23][24][25][26][27][28][29][30][31][32][33][34][35][36]. Only the stiffness of the shaft is considered in the discrete system model, not its inertia.…”
Section: Introductionmentioning
confidence: 99%
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“…Several models are available in literature for the study of rotor system vibrations. They can be categorized into: (i) discrete or lumped parameter model There is a considerable number of literatures on the analysis of continuous rotor systems [6][7][8][9][10][11][12][13][14][15][16][17][18][19][20][21][22] wherein the inertia of the shaft is also considered along with the inertia of the disc. In the continuous model, the governing equations of the shaft-rotor system are first derived in the form of partial differential equations (PDE's) either by using Lagrange's principle Galerkin method [6, 18, 21, 24, 28], or Raleigh-ritz method [3, 9, 11, 16], or any other dimensionality reduction technique.…”
Section: Introductionmentioning
confidence: 99%