BUCKLING TEMPERATURE ANALYSIS OF LAMINATED COMPOSITE PLATES WITH CIRCULAR AND SEMICIRCULAR HOLES

Savaş Evran

doi:10.18038/estubtda.614472

EN

BUCKLING TEMPERATURE ANALYSIS OF LAMINATED COMPOSITE PLATES WITH CIRCULAR AND SEMICIRCULAR HOLES

Abstract

This statistical and numerical study deals with buckling temperature behavior of laminated composite plates with central circular and semicircular holes. Numerical buckling temperature analyses were performed using finite element software ANSYS based on Taguchi L18 orthogonal array. The plates were designed from graphite/epoxy systems. Fiber orientation angles and cutout shapes of the plates were assumed to be the control factors. Analysis of signal-to-noise ratio was used in order to investigate of the effects of fiber orientation angles and cutout shapes on the critical buckling temperature of the plates. Also, analysis of variance was performed in order to see percentage contribution rates and significance levels of control factors.

Keywords

laminated composite,cutout,buckling temperature,ply orientation,FEA

Supporting Institution

Research Fund of the Canakkale Onsekiz Mart University

Project Number

3017

Thanks

The research described in this paper was financially supported by the Research Fund of the Canakkale Onsekiz Mart University. Project Number: 3017

References

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Details

Primary Language

English

Subjects

Engineering

Journal Section

Research Article

Authors

Savaş Evran ^*
0000-0002-7512-5997
Türkiye

Publication Date

March 31, 2020

Submission Date

September 2, 2019

Acceptance Date

March 27, 2020

Published in Issue

Year 2020 Volume: 21 Number: 1

DOI

https://doi.org/10.18038/estubtda.614472

IZ

https://izlik.org/JA87JH56DN

APA

Evran, S. (2020). BUCKLING TEMPERATURE ANALYSIS OF LAMINATED COMPOSITE PLATES WITH CIRCULAR AND SEMICIRCULAR HOLES. Eskişehir Technical University Journal of Science and Technology A - Applied Sciences and Engineering, 21(1), 173-181. https://doi.org/10.18038/estubtda.614472

AMA

1.Evran S. BUCKLING TEMPERATURE ANALYSIS OF LAMINATED COMPOSITE PLATES WITH CIRCULAR AND SEMICIRCULAR HOLES. Estuscience - Se. 2020;21(1):173-181. doi:10.18038/estubtda.614472

Chicago

Evran, Savaş. 2020. “BUCKLING TEMPERATURE ANALYSIS OF LAMINATED COMPOSITE PLATES WITH CIRCULAR AND SEMICIRCULAR HOLES”. Eskişehir Technical University Journal of Science and Technology A - Applied Sciences and Engineering 21 (1): 173-81. https://doi.org/10.18038/estubtda.614472.

EndNote

Evran S (March 1, 2020) BUCKLING TEMPERATURE ANALYSIS OF LAMINATED COMPOSITE PLATES WITH CIRCULAR AND SEMICIRCULAR HOLES. Eskişehir Technical University Journal of Science and Technology A - Applied Sciences and Engineering 21 1 173–181.

IEEE

[1]S. Evran, “BUCKLING TEMPERATURE ANALYSIS OF LAMINATED COMPOSITE PLATES WITH CIRCULAR AND SEMICIRCULAR HOLES”, Estuscience - Se, vol. 21, no. 1, pp. 173–181, Mar. 2020, doi: 10.18038/estubtda.614472.

ISNAD

Evran, Savaş. “BUCKLING TEMPERATURE ANALYSIS OF LAMINATED COMPOSITE PLATES WITH CIRCULAR AND SEMICIRCULAR HOLES”. Eskişehir Technical University Journal of Science and Technology A - Applied Sciences and Engineering 21/1 (March 1, 2020): 173-181. https://doi.org/10.18038/estubtda.614472.

JAMA

1.Evran S. BUCKLING TEMPERATURE ANALYSIS OF LAMINATED COMPOSITE PLATES WITH CIRCULAR AND SEMICIRCULAR HOLES. Estuscience - Se. 2020;21:173–181.

MLA

Evran, Savaş. “BUCKLING TEMPERATURE ANALYSIS OF LAMINATED COMPOSITE PLATES WITH CIRCULAR AND SEMICIRCULAR HOLES”. Eskişehir Technical University Journal of Science and Technology A - Applied Sciences and Engineering, vol. 21, no. 1, Mar. 2020, pp. 173-81, doi:10.18038/estubtda.614472.

Vancouver

1.Savaş Evran. BUCKLING TEMPERATURE ANALYSIS OF LAMINATED COMPOSITE PLATES WITH CIRCULAR AND SEMICIRCULAR HOLES. Estuscience - Se. 2020 Mar. 1;21(1):173-81. doi:10.18038/estubtda.614472

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