Abstract
This paper describes a review of the relevant literature about mistuning problems in bladed disc systems, and their implications for the uncertainty propagation associated to the dynamics of aeroengine systems. An emphasis of the review is placed on the developments of the multi-scale computational techniques to increase the computational efficiency for the linear mistuning analysis, especially with the respect to the reduced order modeling techniques and uncertainty quantification methods. The non-linearity phenomena are not considered in this paper. The first two parts describe the fundamentals of the mechanics of tuned and mistuned bladed discs, followed by a review of critical research efforts performed on the development of reduced order rotor models. The focus of the fourth part is on the review of efficient simulation methods for the stochastic analysis of mistuned bladed disc systems. After that, we will finally provide a view of the current state of the art associated to efficient inversion methods for the stochastic analysis, followed by a summary.
| Original language | English |
|---|---|
| Pages (from-to) | 71-90 |
| Number of pages | 20 |
| Journal | Mechanical Systems and Signal Processing |
| Volume | 87 |
| Issue number | Part A |
| Early online date | 6 Nov 2016 |
| DOIs | |
| Publication status | Published - 15 Mar 2017 |
Funding
The authors would like to acknowledge the support of Rolls-Royce plc for the support of this research through the Composites University Technology Centre (UTC) at the University of Bristol, UK. Special acknowledgement goes also to the Strategic Investment in Low carbon Engine Technology (SILOET) programme supported by Rolls-Royce plc and Technology Strategy Board (TSB), and to the China Scholarship Council. The authors would also like to thank the Reviewers for their useful suggestions.
Keywords
- blades mistuning
- computational methods
- review
- rotordynamics
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