Rub-Impact Dynamics of Offset Disc Rotor with Imbalance and Loosening Pedestal-Reference-Cited by-同舟云学术

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Rub-Impact Dynamics of Offset Disc Rotor with Imbalance and Loosening Pedestal

Published:2024-05 Issue:3 Volume:37 Page:
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Nan Guofang¹,Chen Xu²,Jiang Shan²,Yao Xia²

Affiliation:

1. Associate Professor, School of Energy and Power Engineering, Univ. of Shanghai for Science and Technology, Shanghai 200093, PR China (corresponding author).

2. Graduate Student, School of Energy and Power Engineering, Univ. of Shanghai for Science and Technology, Shanghai 200093, PR China.

Publisher

American Society of Civil Engineers (ASCE)

Link

https://ascelibrary.org/doi/pdf/10.1061/JAEEEZ.ASENG-5425

Reference22 articles.

1. Damage detection techniques for wind turbine blades: A review

2. Nonlinear responses of a dual-rotor system with rub-impact fault subject to interval uncertain parameters

3. Bifurcation and stability analysis of a nonlinear rotor system subjected to constant excitation and rub-impact

4. Bifurcation analysis for 2:1 and 3:1 super-harmonic resonances of an aircraft cracked rotor system due to maneuver load

5. An effective crack position diagnosis method for the hollow shaft rotor system based on the convolutional neural network and deep metric learning

Cited by 1 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Vibration characteristics of rotor system with coupling misalignment and disc-shaft nonlinear contact;Mechanical Systems and Signal Processing;2025-01

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