The dynamic unabalance response and transient motion of the single mass Jeffcott rotor in elastic bearings mounted on damped, flexible supports are discussed. A steady state analysis of the shaft and the bearing housing motion was made by assuming synchronous precession of the system. The conditions under which the support system would act as a dynamic vibration absorber at the rotor critical speed were studied. Plots of the rotor and support amplitudes, phase angles, and forces transmitted were evaluated by the computer and the performance curves were plotted by an automatic plotter unit. Curves are presented on the optimization of the support housing characteristics of attenuate the rotor synchronous unbalance response
PaperPg. 142-147.A study is presented of a simple shaft configuration. This study shows the relative...
This thesis presents a comprehensive analysis of a multi-rotor bearing system, that includes realist...
The unbalance and time varying loading are the principal sources of lateral vibrations of rotors and...
The equations of motion necessary to compute the transient response of multi-mass flexible rotors ar...
Discussed is a magnetic bearing which was designed and tested in a flexible rotor both as support be...
Introduction Vibration of aircraft engines is still an important problem for today. In order to damp...
The generalized dynamic equations of motion were obtained by the direct stiffness method for multima...
An analysis and a computer program for determining the steady-state response of a general rotor-bear...
This paper investigates the steady-state responses of a rotor system supported by auxiliary bearings...
A method of analyzing the first mode stability and unbalance response of multimass flexible rotors i...
This study examines the response of a flexible rotor supported by load sharing between linear bearin...
A series of simulated blade loss tests are reported on a test rotor designed to operate above its se...
Downloaded Fthen used to create equivalent foundation models. An alternative method to include the d...
An analysis and a computer program for determining the steady-state response of a general rotor-bear...
Rolling-element bearing forces vary nonlinearly with bearing deflection. Thus an accurate rotordynam...
PaperPg. 142-147.A study is presented of a simple shaft configuration. This study shows the relative...
This thesis presents a comprehensive analysis of a multi-rotor bearing system, that includes realist...
The unbalance and time varying loading are the principal sources of lateral vibrations of rotors and...
The equations of motion necessary to compute the transient response of multi-mass flexible rotors ar...
Discussed is a magnetic bearing which was designed and tested in a flexible rotor both as support be...
Introduction Vibration of aircraft engines is still an important problem for today. In order to damp...
The generalized dynamic equations of motion were obtained by the direct stiffness method for multima...
An analysis and a computer program for determining the steady-state response of a general rotor-bear...
This paper investigates the steady-state responses of a rotor system supported by auxiliary bearings...
A method of analyzing the first mode stability and unbalance response of multimass flexible rotors i...
This study examines the response of a flexible rotor supported by load sharing between linear bearin...
A series of simulated blade loss tests are reported on a test rotor designed to operate above its se...
Downloaded Fthen used to create equivalent foundation models. An alternative method to include the d...
An analysis and a computer program for determining the steady-state response of a general rotor-bear...
Rolling-element bearing forces vary nonlinearly with bearing deflection. Thus an accurate rotordynam...
PaperPg. 142-147.A study is presented of a simple shaft configuration. This study shows the relative...
This thesis presents a comprehensive analysis of a multi-rotor bearing system, that includes realist...
The unbalance and time varying loading are the principal sources of lateral vibrations of rotors and...