Damage Identification of Rotating Blades Based on Fuzzy C-Means and Frequency Response Function Curvature Methods
Rotor blades are one of the key components of helicopter. If the blades are damaged, the safety and reliability of the helicopter will be seriously affected. Therefore, it is necessary to investigate the damage identification of the rotating blades. In this paper, a rotating cantilever beam is used...
Saved in:
Main Authors: | Ruize Cui, Zefeng Wang, Zhiguang Song |
---|---|
Format: | Article |
Language: | English |
Published: |
Wiley
2023-01-01
|
Series: | International Journal of Aerospace Engineering |
Online Access: | http://dx.doi.org/10.1155/2023/6011397 |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Similar Items
-
Wavelet Transform-Based Damage Identification in Bladed Disks and Rotating Blades
by: P. Rajendran, et al.
Published: (2018-01-01) -
Links between Main Frequencies of Established Rotating Stall and Rotational Frequencies and/or Blade Passing Frequencies
by: Yeshayahou Levy, et al.
Published: (2013-01-01) -
Identification of Damage in a Beam Structure by Using Mode Shape Curvature Squares
by: S. Rucevskis, et al.
Published: (2010-01-01) -
False Financial Statement Identification Based on Fuzzy C-Means Algorithm
by: Jixiao Li
Published: (2021-01-01) -
Identification of Incipient Damage Using High-Frequency Vibrational Responses
by: Maosen Cao, et al.
Published: (2015-01-01)