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22778

A New Closed Form Equation to Design Laminated Composite Tubes with Specified Torsional Stiffness

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Last updated: 04 Jan 2025

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Abstract

Abstract: A New theoretical formula is derived to calculate the torsional stiffness of both thin and thick-walled laminated composite tubes of [θ/-θ]n configuration. This equation can also be used to design the composite tube with a specified value of torsional stiffness accurately and simply. A numerical example is presented to illustrate the design procedure. The method is validated using the results obtained from an accurate method based on three-dimensional elasticity theory from the literature.

DOI

10.21608/asat.2017.22778

Authors

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A.

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Musrati

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M.

Affiliation

Libyan Armed Forces, Libya.

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First Name

M.

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El-Geuchy

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I.

Affiliation

Egyptian Armed Forces, Egypt.

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A.

Last Name

Al-Soualy

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A.

Affiliation

Higher Technological Institute, 10th Ramadan; Egypt.

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First Name

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Hussein

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E.

Affiliation

Egyptian Armed Forces, Egypt.

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Volume

17

Article Issue

AEROSPACE SCIENCES & AVIATION TECHNOLOGY, ASAT - 17 – April 11 - 13, 2017

Related Issue

4266

Issue Date

2017-04-01

Receive Date

2018-12-24

Publish Date

2017-04-01

Page Start

1

Page End

9

Print ISSN

2090-0678

Online ISSN

2636-364X

Article File

ASAT_Volume 17_Issue AEROSPACE SCIENCES & AVIATION TECHNOLOGY, ASAT - 17 &nd….pdf

PDF . 762.1kB

Link

https://asat.journals.ekb.eg/article_22778.html

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https://asat.journals.ekb.eg/service?article_code=22778

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78

Publication Type

Journal

Publication Title

International Conference on Aerospace Sciences and Aviation Technology

Publication Link

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

MainTitle

A New Closed Form Equation to Design Laminated Composite Tubes with Specified Torsional Stiffness

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Article

Created At

22 Jan 2023