NASA NTRS ยท 19860052333
Characteristics pertaining to a stiffness cross-coupled Jeffcott model
Abstract
Rotordynamic studies of complex systems utilizing multiple degree-of-freedom analysis have been performed to understand response, loads, and stability. In order to understand the fundamental nature of rotordynamic response, the Jeffcott rotor model has received wide attention. The purpose of this paper is to provide a generic rotordynamic analysis of a stiffness cross-coupled Jeffcott rotor model to illustrate characteristics of a second order stiffness-coupled linear system. The particular characteristics investigated were forced response, force vector diagrams, response orbits, and stability. Numerical results were achieved through a fourth order Runge-Kutta method for solving differential equations and the Routh Hurwitz stability criterion. The numerical results were verified to an exact mathematical solution for the steady state response.
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Spanyer, K. L.. 1985-09-01. Characteristics pertaining to a stiffness cross-coupled Jeffcott model. https://ntrs.nasa.gov/citations/19860052333
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