Statistical blade tip timing measurement, Part II: High-order cumulant architecture
Author:
Funder
Fundamental Research Funds for the Central Universities
National Natural Science Foundation of China
Publisher
Elsevier BV
Reference44 articles.
1. Reliability analysis of aero-engine compressor rotor system considering cruise characteristics;Zhao;IEEE Trans. Reliab.,2019
2. Failure analysis of an un-cooled turbine blade in an aero gas turbine engine;Mishra;Eng. Fail. Anal.,2017
3. A class of methods for the analysis of blade tip timing data from bladed assemblies undergoing simultaneous resonances—Part I: Theoretical development;Gallego-Garrido;Int. J. Rotating Mach.,2007
4. Method to improve the blade tip-timing accuracy of fiber bundle sensor under varying tip clearance;Duan;Opt. Eng., Bellingham,2016
5. Tip-timing measurements and numerical analysis of last-stage steam turbine mistuned bladed disc during run-down;Rzadkowski;J. Vib. Eng. Technol.,2020
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