24842

MULTILEVEL OPTIMIZATION OF LAMINATED COMPOSITE STRUCTURES

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Last updated: 04 Jan 2025

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Abstract

This paper presents a multilevel approach to the optimal design of laminated composites with consideration of natural frequency constraints The Ply thicknesses and orientations are designed to minimize the volumes of plates subjected to constraints on the first natural frequency. The optimization process is carried out in a dual scheme. In the first optimization level the optimal ply orientations which give the maximum natural frequency are determined. In the second level the optimal ply thicknesses are determined so as to minimize the structural weight, while maintaining the ply angles obtained in the first level. The process is repeated several times until convergence is obtained. Weight minimization is performed by two different methods: the constrained gradient travel method and the optimality criterion method.

DOI

10.21608/asat.2001.24842

Keywords

Optimum, Laminated Composite Plate, Dynamic and Static

Authors

First Name

NASR

Last Name

N.

MiddleName

A.

Affiliation

1General Manger A.O.I. Aircraft Engine Factory, Helwan, Cairo, Egypt.

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Orcid

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First Name

NEGM

Last Name

M.

MiddleName

H.

Affiliation

Professor of Aircraft Structures, Aerospace Engineering Department, Cairo University.

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Volume

9

Article Issue

ASAT Conference, 8-10 May 2001

Related Issue

4547

Issue Date

2001-05-01

Receive Date

2019-01-16

Publish Date

2001-05-01

Page Start

1

Page End

16

Print ISSN

2090-0678

Online ISSN

2636-364X

Link

https://asat.journals.ekb.eg/article_24842.html

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https://asat.journals.ekb.eg/service?article_code=24842

Order

37

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

MULTILEVEL OPTIMIZATION OF LAMINATED COMPOSITE STRUCTURES

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Article

Created At

22 Jan 2023