Vibration response analysis of blade-disk dovetail structure under blade tip rubbing condition
Author:
Affiliation:
1. School of Mechanical Engineering and Automation, Northeastern University, Shenyang, Liaoning PR China
2. Shenyang Blower Works Group Corporation, Shenyang, PR China
Abstract
Publisher
SAGE Publications
Subject
Mechanical Engineering,Mechanics of Materials,Aerospace Engineering,Automotive Engineering,General Materials Science
Link
http://journals.sagepub.com/doi/pdf/10.1177/1077546315575835
Reference25 articles.
1. Rotor Casing Contact Phenomenon in Rotor Dynamics — Literature Survey
2. Effect of three-dimensional loading on macroscopic fretting aspects of an aero-engine blade–disc dovetail interface
3. Assessment of reduced models for the detection of modal interaction through rotor stator contacts
4. Multiscale computation of fretting wear at the blade/disk interface
5. Rotor to stator contacts in turbomachines. Review and application
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