Araştırma Makalesi

DETERMINATION OF THE THEORATICAL BUCKLING LOAD OF HYBRID COMPOSITE LAMINATES HAVING DIFFERENT HOLE DIAMETERS THROUGH TAGUCHI-BASED FUZZY MODEL

Cilt: 67 Sayı: 724 30 Eylül 2026
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DETERMINATION OF THE THEORATICAL BUCKLING LOAD OF HYBRID COMPOSITE LAMINATES HAVING DIFFERENT HOLE DIAMETERS THROUGH TAGUCHI-BASED FUZZY MODEL

Öz

This study examined the determination of theoretical buckling load of hybrid composite laminates with different hole diameters using the Taguchi-based fuzzy optimization method. In the Taguchi-based fuzzy method, the buckling parameters in the theoretical approach were used as input data, and the critical buckling load value was considered the output. Multiple Performance Characteristics Index (MPCI) was utilized for determining optimization results. Moreover, theoretical results verified by experimental and numerical approaches. In the experimental approach, the hybrid composite laminates (HCGFRE) manufactured by sequential sequencing of plain woven glass fiber reinforced epoxy (GFRE) and plain woven carbon fiber reinforced laminates (CFRE). Tests were carried out at a constant loading rate of 1 mm/min at room temperature. In numerical analysis, eigenvalue buckling was performed using Ansys finite element program. Composite laminates were formed utilizing Composite PrepPost (ACP) sub-module. Eventually, it was observed that using the Taguchi-based fuzzy method to determine the critical buckling load of hybrid composite laminates is consistent with both experimental and numerical approaches in terms of results

Anahtar Kelimeler

Kaynakça

  1. Achour B., Ouinas D., Touahmia M. and Boukendakdji M.. (2018). Buckling of hybrid composite carbon/epoxy/aluminum plates with cutouts. Eng Technol Appl Sci Res, 8(1) : 2393-2398. https://doi.org/10.48084/etasr.1224
  2. Allahbakhsh H. and Dadrasi A. ( 2012). Buckling analysis of laminated composite panel with elliptical cutout subject to axial compression. Modell Simul Eng,1: 171953. https://doi.org/10.1155/2012/171953
  3. Altan MF and Kartal ME.(2009).Investigation of buckling behavior of laminated reinforced concrete plates with central rectangular hole using finite element method. Mater Des 30: 2243–2249. https://doi.org/10.1016/j.matdes.2008.08.026
  4. ANSYS, Introduction to Ansys Composite PrepPost (ACP). (2022, accessed 1 January 2022).
  5. Arman Y., Zor M. and Aksoy S.(2006). Determination of critical delamination diameter of laminate composite plates under buckling loads. Compos Sci Technol, 66:2945–2953. https://doi.org/10.1016/j.compscitech.2006.02.014
  6. ASTM D8511, Standard Guide for Design and Analysis of Local Buckling and Crippling Test Specimen accessed 20 September 2023.
  7. Boga C., Koroglu T.(2021). Proper estimation of surface roughness using hybrid intelligence based on artificial neural network and genetic algorithm. J Manuf Proc, 70:560-569 https://doi.org/10.1016/j.jmapro.2021.08.062
  8. Damghani M., Pir RA, Murphy A. and Fotouhet M.(2022). Experimental and numerical study of hybrid (CFRP-GFRP) composite laminates containing circular cut-outs under shear loading. Thin-Walled Struct, 179:109752. https://doi.org/10.1016/j.tws.2022.109752

Ayrıntılar

Birincil Dil

İngilizce

Konular

Katı Mekanik, Makine Mühendisliğinde Optimizasyon Teknikleri, Kompozit ve Hibrit Malzemeler

Bölüm

Araştırma Makalesi

Yayımlanma Tarihi

30 Eylül 2026

Gönderilme Tarihi

14 Ağustos 2025

Kabul Tarihi

20 Şubat 2026

Yayımlandığı Sayı

Yıl 2026 Cilt: 67 Sayı: 724

Kaynak Göster

APA
Erbayrak, E., & Erbayrak, S. (2026). DETERMINATION OF THE THEORATICAL BUCKLING LOAD OF HYBRID COMPOSITE LAMINATES HAVING DIFFERENT HOLE DIAMETERS THROUGH TAGUCHI-BASED FUZZY MODEL. Mühendis ve Makina, 67(724), 355-377. https://doi.org/10.46399/muhendismakina.1764046
AMA
1.Erbayrak E, Erbayrak S. DETERMINATION OF THE THEORATICAL BUCKLING LOAD OF HYBRID COMPOSITE LAMINATES HAVING DIFFERENT HOLE DIAMETERS THROUGH TAGUCHI-BASED FUZZY MODEL. Mühendis ve Makina. 2026;67(724):355-377. doi:10.46399/muhendismakina.1764046
Chicago
Erbayrak, Engin, ve Seda Erbayrak. 2026. “DETERMINATION OF THE THEORATICAL BUCKLING LOAD OF HYBRID COMPOSITE LAMINATES HAVING DIFFERENT HOLE DIAMETERS THROUGH TAGUCHI-BASED FUZZY MODEL”. Mühendis ve Makina 67 (724): 355-77. https://doi.org/10.46399/muhendismakina.1764046.
EndNote
Erbayrak E, Erbayrak S (01 Eylül 2026) DETERMINATION OF THE THEORATICAL BUCKLING LOAD OF HYBRID COMPOSITE LAMINATES HAVING DIFFERENT HOLE DIAMETERS THROUGH TAGUCHI-BASED FUZZY MODEL. Mühendis ve Makina 67 724 355–377.
IEEE
[1]E. Erbayrak ve S. Erbayrak, “DETERMINATION OF THE THEORATICAL BUCKLING LOAD OF HYBRID COMPOSITE LAMINATES HAVING DIFFERENT HOLE DIAMETERS THROUGH TAGUCHI-BASED FUZZY MODEL”, Mühendis ve Makina, c. 67, sy 724, ss. 355–377, Eyl. 2026, doi: 10.46399/muhendismakina.1764046.
ISNAD
Erbayrak, Engin - Erbayrak, Seda. “DETERMINATION OF THE THEORATICAL BUCKLING LOAD OF HYBRID COMPOSITE LAMINATES HAVING DIFFERENT HOLE DIAMETERS THROUGH TAGUCHI-BASED FUZZY MODEL”. Mühendis ve Makina 67/724 (01 Eylül 2026): 355-377. https://doi.org/10.46399/muhendismakina.1764046.
JAMA
1.Erbayrak E, Erbayrak S. DETERMINATION OF THE THEORATICAL BUCKLING LOAD OF HYBRID COMPOSITE LAMINATES HAVING DIFFERENT HOLE DIAMETERS THROUGH TAGUCHI-BASED FUZZY MODEL. Mühendis ve Makina. 2026;67:355–377.
MLA
Erbayrak, Engin, ve Seda Erbayrak. “DETERMINATION OF THE THEORATICAL BUCKLING LOAD OF HYBRID COMPOSITE LAMINATES HAVING DIFFERENT HOLE DIAMETERS THROUGH TAGUCHI-BASED FUZZY MODEL”. Mühendis ve Makina, c. 67, sy 724, Eylül 2026, ss. 355-77, doi:10.46399/muhendismakina.1764046.
Vancouver
1.Engin Erbayrak, Seda Erbayrak. DETERMINATION OF THE THEORATICAL BUCKLING LOAD OF HYBRID COMPOSITE LAMINATES HAVING DIFFERENT HOLE DIAMETERS THROUGH TAGUCHI-BASED FUZZY MODEL. Mühendis ve Makina. 01 Eylül 2026;67(724):355-77. doi:10.46399/muhendismakina.1764046

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ISSN : 1300-3402

E-ISSN : 2667-7520