Management of the variability of vibration response levels in mistuned bladed discs using robust design concepts. Part 1-Reference-Cited by-同舟云学术

Management of the variability of vibration response levels in mistuned bladed discs using robust design concepts. Part 1

Published:2010-11 Issue:8 Volume:24 Page:2777-2791
ISSN:0888-3270
Container-title:Mechanical Systems and Signal Processing
language:en
Short-container-title:Mechanical Systems and Signal Processing

Author:

Chan Y.-J.,Ewins D.J.

Publisher

Elsevier BV

Subject

Computer Science Applications,Mechanical Engineering,Aerospace Engineering,Civil and Structural Engineering,Signal Processing,Control and Systems Engineering

Reference27 articles.

1. Flutter and resonant vibration characteristics of engine blades;Srinivasan;Transactions of the ASME. Journal of Engineering for Gas Turbines and Power,1997

2. Development of the British Gas Turbine Unit;Constant,1947

3. Analysis of the worst mistuning patterns in bladed disk assemblies;Petrov;Transactions of the ASME. Journal of Turbomachinery,2003

4. The Superalloys: Fundamentals and Applications;Reed,2006

5. B. Garrison, High cycle fatigue (HCF) science and technology program 2000 annual report, Technical Report AFRL-PR-WP-TR-2001–2010, Propulsion Directorate, Air Force Research Laboratory, Air Force Material Command, Wright-Patterson AFB, 2000.

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