Determination of Contact Stiffness and Damping of a Tie-Bolt Rotor with Interference Fits Using Model Updating with Thin-Layer Elements
Tie-bolt rotors are commonly applied in aeroengines and gas turbines, and interference fits ensure accurate positioning for disk assembling. This paper presents experimental and numerical studies on the stiffness and damping properties of a tie-bolt rotor with interference fits under different prelo...
Saved in:
Main Authors: | Pu Li, Qi Yuan |
---|---|
Format: | Article |
Language: | English |
Published: |
Wiley
2020-01-01
|
Series: | Shock and Vibration |
Online Access: | http://dx.doi.org/10.1155/2020/8872401 |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Similar Items
-
Research on the Simulation Method for Equivalent Stiffness of Bolted Connection Thin Plate Structures
by: Zhe Chen, et al.
Published: (2024-01-01) -
Updating Stiffness and Hysteretic Damping Matrices Using Measured Modal Data
by: Jiashang Jiang, et al.
Published: (2018-01-01) -
Nonlinear Analysis of Rod Fastened Rotor under Nonuniform Contact Stiffness
by: Jiaqi Li, et al.
Published: (2020-01-01) -
Damping Prediction of Structures with Bolted Joints
by: Lothar Gaul, et al.
Published: (2010-01-01) -
Analysis of Layered Composite Beam to Underwater Shock Including Structural Damping and Stiffness Effects
by: S.W. Gong, et al.
Published: (2002-01-01)