Computational Studies of the Unbalance Response of a Whole Aero-Engine Model With Squeeze-Film Bearings
Author:
Affiliation:
1. School of Mechanical, Aerospace and Civil Engineering, University of Manchester, Manchester, M60 1QD, UK
Abstract
Publisher
ASME International
Subject
Mechanical Engineering,Energy Engineering and Power Technology,Aerospace Engineering,Fuel Technology,Nuclear Energy and Engineering
Link
http://asmedigitalcollection.asme.org/gasturbinespower/article-pdf/doi/10.1115/1.3159381/5509531/032504_1.pdf
Reference11 articles.
1. An Impulsive Receptance Technique for the Time Domain Computation of the Vibration of a Whole Aero-Engine Model With Nonlinear Bearings;Hai;J. Sound Vib.
2. Non-Linear Modelling of Rotor Dynamic Systems With Squeeze Film Dampers—An Efficient Integrated Approach;Bonello;J. Sound Vib.
3. Analysis of a Flexible Rotor System Including Non-Linear Squeeze Film Damping Using a Finite Element Method;Lim
4. Efficient Computation on the Nonlinear Responses of a Rotating Assembly Incorporating the Squeeze-Film Damper;Chu;Comput. Methods Appl. Mech. Eng.
5. Transient Modal Analysis of Nonlinear Rotor-Bearing Systems;Armentrout;Proc. SPIE
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