Application of Improved Dynamic Substructure Finite Element Model-Based State-Space Techniques in Mistuned Blisks
Aeroengine is a complex mechanical equipment, and it works at high temperature, pressure, rotational-speed, and severe loads. One of the core problems is that the vibration and mistuning of bladed disk lead to failure and affect the safety and reliability of aeroengine. Previously, one sector taken...
Saved in:
Main Authors: | Bin Bai, Chuan hui Zhang, Guangwei Zhu, Qi liang Wu |
---|---|
Format: | Article |
Language: | English |
Published: |
Wiley
2020-01-01
|
Series: | International Journal of Aerospace Engineering |
Online Access: | http://dx.doi.org/10.1155/2020/8817531 |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Similar Items
-
Application of Probabilistic and Nonprobabilistic Hybrid Reliability Analysis Based on Dynamic Substructural Extremum Response Surface Decoupling Method for a Blisk of the Aeroengine
by: Bin Bai, et al.
Published: (2017-01-01) -
On the Forced Response of Harmonically and Partially
Mistuned Bladed Disks. Part I: Harmonic Mistuning
by: Marc P. Mignolet, et al.
Published: (2000-01-01) -
On the Forced Response of Harmonically and Partially Mistuned
Bladed Disks. Part II: Partial Mistuning and Applications
by: Marc P. Mignolet, et al.
Published: (2000-01-01) -
Vibration Analysis of Aeroengine Blisk Structure Based on a Prestressed CMS Super-Element Method
by: Zhijun Li, et al.
Published: (2016-01-01) -
On Antiresonance in the Forced Response of Mistuned Bladed Disks
by: Keith Jones, et al.
Published: (2003-01-01)