This paper presents experimental results on the non-linear vibration response of a rotating assembly comprising a rotor, flexible bearing housing and oil film damper. For the latter, due consideration is given to the effects of oil-supply pressure, film-rupture pressure and end sealing. The results are compared with predictions based on the Harmonic Balance principle described in a complementary paper (1).
Experimental Investigation into the Vibration Response of an Aero-Engine Rotor-Damper Assembly
1994-01-01
15 pages
Article (Journal)
Electronic Resource
English
Experimental investigation into the vibration response of an aero-engine rotor-damper assembly
Online Contents | 1994
|The efficient computation of the vibration response of an aero-engine rotor-damper assembly
Online Contents | 1994
|The Efficient Computation of the Vibration Response of an Aero-Engine Rotor-Damper Assembly
SAGE Publications | 1994
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