2008
DOI: 10.1115/1.3007973
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Numerical Method and Bifurcation Analysis of Jeffcott Rotor System Supported in Gas Journal Bearings

Abstract: From the viewpoint of nonlinear dynamics, the stability and bifurcation of the rotor dynamical system supported in gas bearings are investigated. First, the dynamical model of gas bearing-Jeffcott rotor system is given, and the finite element method is used to approach the unsteady Reynolds equation in order to obtain gas film forces. Then, the method for stability analysis of the unbalance response of the rotor system is developed in combination with the Newmark-based direct integral method and Floquet theory… Show more

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Cited by 28 publications
(18 citation statements)
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“…[1][2][3][4]). This means that the pressure at each mesh point is a state variable and the discretised RE will be a set of temporal differential equations (TDEs i.e.…”
Section: Introductionmentioning
confidence: 99%
“…[1][2][3][4]). This means that the pressure at each mesh point is a state variable and the discretised RE will be a set of temporal differential equations (TDEs i.e.…”
Section: Introductionmentioning
confidence: 99%
“…(18) has to be transformed to the state-space in order to be integrable by standard numerical solvers. The transformation was briefly described in section 2.3.…”
Section: Solution Strategymentioning
confidence: 99%
“…A transient state which occurs in rotor-bearing system when a journal pass the threshold speed is studied in [13], where small amplitude perturbations are assumed in the bearing. The transient state of Jeffcott rotor supported by a gas bearing and accompanying bifurcations are studied in [18].…”
Section: Introductionmentioning
confidence: 99%
“…As observed in [1,2], due to the computational burden so introduced, the simultaneous solution of the state equations of the air film, foil and rotor has typically been avoided. In works such as [3][4][5][6][7][8] the air-film ODEs are uncoupled from the foil and rotor ODEs and approximated as algebraic equations; these latter equations were solved iteratively for the current pressure distribution using the rotor state variables at the previous time step [1,2].…”
Section: Introductionmentioning
confidence: 99%
“…The use of Finite Difference (FD)/Finite Element (FE)/Control Volume methods [3][4][5][6][7][8][9] to discretize the RE over the air film, creates a grid of points representing the pressure field, turning the RE into a set of first order ordinary differential equations (ODEs) with time as the independent variable (state equations). As observed in [1,2], due to the computational burden so introduced, the simultaneous solution of the state equations of the air film, foil and rotor has typically been avoided.…”
Section: Introductionmentioning
confidence: 99%