An Efficient Optimization of Composite Structures for Vibration Based on Approximation Method

Masaki Kameyama; Masaki Furuta; Hisao Fukunaga; Hideki Sekine

doi:10.1299/kikaic.66.2912

An Efficient Optimization of Composite Structures for Vibration Based on Approximation Method

Masaki Kameyama, Masaki Furuta, Hisao Fukunaga, Hideki Sekine

ENG - Aerospace Engineering

Research output: Contribution to journal › Article › peer-review

Abstract

The present paper shows an efficient optimization approach on composite structures for vibration where layer angles in addition to layer thicknesses are used as design variables. A high-quality approximation method of natural frequencies with respect to layer angle and layer thickness is proposed. First in the present paper, several approximate methods of natural frequencies after design variation are compared. Next, an approximation method is then applied to a minimum weight design of cantilevered laminated plates under multiple frequency constraints. The validity of the present approach is verified through the numerical examples of laminated plates.

Original language	English
Pages (from-to)	2912-2918
Number of pages	7
Journal	Nihon Kikai Gakkai Ronbunshu, C Hen/Transactions of the Japan Society of Mechanical Engineers, Part C
Volume	66
Issue number	649
DOIs	https://doi.org/10.1299/kikaic.66.2912
Publication status	Published - 2000

Keywords

Approximation Method
Composite Material
Free Vibration
Lamination Parameter
Optimum Design
Reanalysis Method
Sensitivity Analysis

ASJC Scopus subject areas

Mechanics of Materials
Mechanical Engineering
Industrial and Manufacturing Engineering

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An Efficient Optimization of Composite Structures for Vibration Based on Approximation Method. / Kameyama, Masaki; Furuta, Masaki; Fukunaga, Hisao; Sekine, Hideki.

In: Nihon Kikai Gakkai Ronbunshu, C Hen/Transactions of the Japan Society of Mechanical Engineers, Part C, Vol. 66, No. 649, 2000, p. 2912-2918.

Research output: Contribution to journal › Article › peer-review

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abstract = "The present paper shows an efficient optimization approach on composite structures for vibration where layer angles in addition to layer thicknesses are used as design variables. A high-quality approximation method of natural frequencies with respect to layer angle and layer thickness is proposed. First in the present paper, several approximate methods of natural frequencies after design variation are compared. Next, an approximation method is then applied to a minimum weight design of cantilevered laminated plates under multiple frequency constraints. The validity of the present approach is verified through the numerical examples of laminated plates.",

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AU - Fukunaga, Hisao

AU - Sekine, Hideki

PY - 2000

Y1 - 2000

N2 - The present paper shows an efficient optimization approach on composite structures for vibration where layer angles in addition to layer thicknesses are used as design variables. A high-quality approximation method of natural frequencies with respect to layer angle and layer thickness is proposed. First in the present paper, several approximate methods of natural frequencies after design variation are compared. Next, an approximation method is then applied to a minimum weight design of cantilevered laminated plates under multiple frequency constraints. The validity of the present approach is verified through the numerical examples of laminated plates.

AB - The present paper shows an efficient optimization approach on composite structures for vibration where layer angles in addition to layer thicknesses are used as design variables. A high-quality approximation method of natural frequencies with respect to layer angle and layer thickness is proposed. First in the present paper, several approximate methods of natural frequencies after design variation are compared. Next, an approximation method is then applied to a minimum weight design of cantilevered laminated plates under multiple frequency constraints. The validity of the present approach is verified through the numerical examples of laminated plates.

KW - Approximation Method

KW - Composite Material

KW - Free Vibration

KW - Lamination Parameter

KW - Optimum Design

KW - Reanalysis Method

KW - Sensitivity Analysis

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JO - Nihon Kikai Gakkai Ronbunshu, C Hen/Transactions of the Japan Society of Mechanical Engineers, Part C

JF - Nihon Kikai Gakkai Ronbunshu, C Hen/Transactions of the Japan Society of Mechanical Engineers, Part C

SN - 0387-5024

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ER -

An Efficient Optimization of Composite Structures for Vibration Based on Approximation Method

Abstract

Keywords

ASJC Scopus subject areas

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