DESIGN OPTIMIZATION OF TORSIONAL CRUSHING BEHAVIOUR OF FIBER METAL LAMINATE THIN-WALLED PRISMATIC STRUCTURES

Thin-walled structures have been extensively studied regarding their behavior under compressive loading, bending, and several studies regarding torsional loading. The application of fiber metal laminate (FML) material to thin-walled structures is proven to improve the performance of thin-walled stru...

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Main Author: Yassar, Naufal
Format: Final Project
Language:Indonesia
Online Access:https://digilib.itb.ac.id/gdl/view/71391
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Institution: Institut Teknologi Bandung
Language: Indonesia
id id-itb.:71391
spelling id-itb.:713912023-02-06T08:59:51ZDESIGN OPTIMIZATION OF TORSIONAL CRUSHING BEHAVIOUR OF FIBER METAL LAMINATE THIN-WALLED PRISMATIC STRUCTURES Yassar, Naufal Indonesia Final Project thin-walled structure, crashworthiness, fiber metal laminate, torsional loading, Taguchi method, analysis of variance INSTITUT TEKNOLOGI BANDUNG https://digilib.itb.ac.id/gdl/view/71391 Thin-walled structures have been extensively studied regarding their behavior under compressive loading, bending, and several studies regarding torsional loading. The application of fiber metal laminate (FML) material to thin-walled structures is proven to improve the performance of thin-walled structures in terms of crashworthiness. The behavior of thin-walled structures made of FML subjected to torsional crushing load was investigated numerically in this study. Two crashworthiness parameters were observed, namely specific initial torsional crushing moment (STi) and specific energy absorption (SEA). Design optimization was carried out using the design for six sigma (DFSS) Taguchi method with the L18 orthogonal array to obtain the combination of parameters that produces the highest STi and SEA values. Several variations of structure parameters, namely metal layer material, fiber reinforced polymer (FRP) material, FML arrangement order, fiber orientation, metal layer thickness, number of fiber layers, cross-sectional shape, and adhesive between the metal layer and fiber layer were determined as control factors. Optimization results show the use of structure with an octagonal cross-sectional shape, Al2024-T3 material, T700/epoxy carbon material, M/F/F/F/M arrangement order, fiber orientation of [+45o/-45o], metal layer thickness of 0.6 mm, the number of FRP layers is 6 pieces, and 105/206 epoxy adhesive can produce the highest STi values. While the optimum parameters for SEA have several differences from the STi optimum parameters, namely Ti-6Al-4V material, fiber orientation of [0o/90o], and epoxy/GNP adhesive. The effect of each parameter on STi and SEA values was evaluated using analysis of variance (ANOVA). Fiber orientation contributed the most to the STi value, which is 34.38%. Meanwhile, the biggest contribution to the SEA value is the order of FML preparation, which is 31.27%. text
institution Institut Teknologi Bandung
building Institut Teknologi Bandung Library
continent Asia
country Indonesia
Indonesia
content_provider Institut Teknologi Bandung
collection Digital ITB
language Indonesia
description Thin-walled structures have been extensively studied regarding their behavior under compressive loading, bending, and several studies regarding torsional loading. The application of fiber metal laminate (FML) material to thin-walled structures is proven to improve the performance of thin-walled structures in terms of crashworthiness. The behavior of thin-walled structures made of FML subjected to torsional crushing load was investigated numerically in this study. Two crashworthiness parameters were observed, namely specific initial torsional crushing moment (STi) and specific energy absorption (SEA). Design optimization was carried out using the design for six sigma (DFSS) Taguchi method with the L18 orthogonal array to obtain the combination of parameters that produces the highest STi and SEA values. Several variations of structure parameters, namely metal layer material, fiber reinforced polymer (FRP) material, FML arrangement order, fiber orientation, metal layer thickness, number of fiber layers, cross-sectional shape, and adhesive between the metal layer and fiber layer were determined as control factors. Optimization results show the use of structure with an octagonal cross-sectional shape, Al2024-T3 material, T700/epoxy carbon material, M/F/F/F/M arrangement order, fiber orientation of [+45o/-45o], metal layer thickness of 0.6 mm, the number of FRP layers is 6 pieces, and 105/206 epoxy adhesive can produce the highest STi values. While the optimum parameters for SEA have several differences from the STi optimum parameters, namely Ti-6Al-4V material, fiber orientation of [0o/90o], and epoxy/GNP adhesive. The effect of each parameter on STi and SEA values was evaluated using analysis of variance (ANOVA). Fiber orientation contributed the most to the STi value, which is 34.38%. Meanwhile, the biggest contribution to the SEA value is the order of FML preparation, which is 31.27%.
format Final Project
author Yassar, Naufal
spellingShingle Yassar, Naufal
DESIGN OPTIMIZATION OF TORSIONAL CRUSHING BEHAVIOUR OF FIBER METAL LAMINATE THIN-WALLED PRISMATIC STRUCTURES
author_facet Yassar, Naufal
author_sort Yassar, Naufal
title DESIGN OPTIMIZATION OF TORSIONAL CRUSHING BEHAVIOUR OF FIBER METAL LAMINATE THIN-WALLED PRISMATIC STRUCTURES
title_short DESIGN OPTIMIZATION OF TORSIONAL CRUSHING BEHAVIOUR OF FIBER METAL LAMINATE THIN-WALLED PRISMATIC STRUCTURES
title_full DESIGN OPTIMIZATION OF TORSIONAL CRUSHING BEHAVIOUR OF FIBER METAL LAMINATE THIN-WALLED PRISMATIC STRUCTURES
title_fullStr DESIGN OPTIMIZATION OF TORSIONAL CRUSHING BEHAVIOUR OF FIBER METAL LAMINATE THIN-WALLED PRISMATIC STRUCTURES
title_full_unstemmed DESIGN OPTIMIZATION OF TORSIONAL CRUSHING BEHAVIOUR OF FIBER METAL LAMINATE THIN-WALLED PRISMATIC STRUCTURES
title_sort design optimization of torsional crushing behaviour of fiber metal laminate thin-walled prismatic structures
url https://digilib.itb.ac.id/gdl/view/71391
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