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198024

Effect of damping material thickness on vibration analysis in pretension layer damping process

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Last updated: 04 Jan 2025

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Abstract

Vibration reduction is a critical necessity in many fields of engineering, technology, and industry. As a result, there is a need for vibration management. To restrict or adjust the system's vibration response, a variety of techniques are employed. In recent years, there has been a lot of enthusiasm for the easy implementation of these vibration-control structures. The damping properties of viscoelastic materials tend to be excellent. Damping is determined by the material's ability to dissipate energy. To minimise the vibration of vibrating surfaces, viscoelastic materials are commonly used. In this study, viscoelastic material (Dyad 606) is applied on the AL plate in the form of free layer damping and pretension layer damping. First aluminium structure using free layer damping and another one using pretension layer damping by applying tension load (two layers of damping plates, one on the top surface of the Al alloy and the other on the lower face). Passive vibration damping of the plate is achieved. These layers are influenced by axial uniform distributed load. The damping behaviour of the AL Plate is discussed in relation to the thickness variation of the pre-tension damping material. The results show that the loss factor and the attenuation percentage of the structure with pretension layer damping are increased as compared to free layer damping. It is also found that the most effective thickness of the damping material to increase the damping capacity of the framework is around half the base plate thickness

DOI

10.1088/1757-899X/1172/1/012006

Authors

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Last Name

Mohamed

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Affiliation

Mechanical Engineering Department, Military Technical College, Cairo, Egypt.

Email

anwer_mohamed@mtc.edu.eg

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First Name

A

Last Name

Omer

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A

Affiliation

Mechanical Engineering Department, Military Technical College, Cairo, Egypt.

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City

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First Name

A

Last Name

Hassan

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Affiliation

Mechanical Engineering Department, Military Technical College, Cairo, Egypt.

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Volume

19

Article Issue

19

Related Issue

27988

Issue Date

2021-04-01

Receive Date

2021-10-04

Publish Date

2021-04-01

Page Start

1

Page End

10

Print ISSN

2090-0678

Online ISSN

2636-364X

Link

https://asat.journals.ekb.eg/article_198024.html

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https://asat.journals.ekb.eg/service?article_code=198024

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8

Type

Original Article

Type Code

737

Publication Type

Journal

Publication Title

International Conference on Aerospace Sciences and Aviation Technology

Publication Link

https://asat.journals.ekb.eg/

MainTitle

Effect of damping material thickness on vibration analysis in pretension layer damping process

Details

Type

Article

Created At

22 Jan 2023