Mechanical Properties of Multi-Layer Woven E-Glass/Epoxy in Variable Fiber-Mat Directions
In this research, the epoxy resin was reinforced by (16 layers) of E-glass fiber woven mat (0^°/90^°) with 50% weight fraction and total thickness (3mm). Using 16 layers was due to the absence of any previous study that used this number of layers at this thickness. It is considered a modern study o...
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middle technical university
2023-06-01
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Online Access: | https://journal.mtu.edu.iq/index.php/MTU/article/view/1176 |
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author | Saif Aldeen Ghafel H. Nasri Salh M. Namer Abdul Jabbar H. Ali |
author_facet | Saif Aldeen Ghafel H. Nasri Salh M. Namer Abdul Jabbar H. Ali |
author_sort | Saif Aldeen Ghafel H. |
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In this research, the epoxy resin was reinforced by (16 layers) of E-glass fiber woven mat (0^°/90^°) with 50% weight fraction and total thickness (3mm). Using 16 layers was due to the absence of any previous study that used this number of layers at this thickness. It is considered a modern study of this style because of the rapid development in modern engineering industries that required lightweight composite materials with high strength and small thickness, which are used in the aerospace industry aviation and other precision engineering industries. The composite material was cut into angles (0^°,5^°,15^°,30^°,45^°) by using CNC water jet culling machine. The tensile test was used to determine the strength of a material ratio to the fiber's direction and by using Vickers hardness to determine the hardness of composite and pure epoxy. The result of pure epoxy (matrix) has the lowest value in tensile strength (σ_UTS), Yong's modulus (E), 0.2% proof yield stress (σ_(0.2%)), modulus of toughness and toughness when compared with a composite material with adding 16 layers of "E-glass fibers". The direction of the fibers with (5^°) of composite has the highest strength, Young's modulus, and 0.2% proof yield stress when compared with (0^°,15^°,30^°,45^°) and pure epoxy. The improvement strength (10.8, 11.8, 9.8, 8.5, 8.3 times) at (0^°,5^°,15^°,30^°,45^°) respectively when compared with pure epoxy. The hardness of composite material improved (220%) relative to pure epoxy. The results show that the best improvement of composite material with fiber's angle (5^°) has the highest results compared with pure epoxy.
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publishDate | 2023-06-01 |
publisher | middle technical university |
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spelling | doaj-art-1d1b4a274ccd4fab8649b54283d17a782025-01-19T11:01:51Zengmiddle technical universityJournal of Techniques1818-653X2708-83832023-06-015210.51173/jt.v5i2.1176Mechanical Properties of Multi-Layer Woven E-Glass/Epoxy in Variable Fiber-Mat DirectionsSaif Aldeen Ghafel H.0Nasri Salh M. Namer1Abdul Jabbar H. Ali2Engineering Technical College - Baghdad, Middle Technical University, Baghdad, IraqEngineering Technical College - Baghdad, Middle Technical University, Baghdad, IraqAl-khawarizmi College of Engineering, University Baghdad, Iraq In this research, the epoxy resin was reinforced by (16 layers) of E-glass fiber woven mat (0^°/90^°) with 50% weight fraction and total thickness (3mm). Using 16 layers was due to the absence of any previous study that used this number of layers at this thickness. It is considered a modern study of this style because of the rapid development in modern engineering industries that required lightweight composite materials with high strength and small thickness, which are used in the aerospace industry aviation and other precision engineering industries. The composite material was cut into angles (0^°,5^°,15^°,30^°,45^°) by using CNC water jet culling machine. The tensile test was used to determine the strength of a material ratio to the fiber's direction and by using Vickers hardness to determine the hardness of composite and pure epoxy. The result of pure epoxy (matrix) has the lowest value in tensile strength (σ_UTS), Yong's modulus (E), 0.2% proof yield stress (σ_(0.2%)), modulus of toughness and toughness when compared with a composite material with adding 16 layers of "E-glass fibers". The direction of the fibers with (5^°) of composite has the highest strength, Young's modulus, and 0.2% proof yield stress when compared with (0^°,15^°,30^°,45^°) and pure epoxy. The improvement strength (10.8, 11.8, 9.8, 8.5, 8.3 times) at (0^°,5^°,15^°,30^°,45^°) respectively when compared with pure epoxy. The hardness of composite material improved (220%) relative to pure epoxy. The results show that the best improvement of composite material with fiber's angle (5^°) has the highest results compared with pure epoxy. https://journal.mtu.edu.iq/index.php/MTU/article/view/1176Multi-LayerWovenFiber-Mat Directions |
spellingShingle | Saif Aldeen Ghafel H. Nasri Salh M. Namer Abdul Jabbar H. Ali Mechanical Properties of Multi-Layer Woven E-Glass/Epoxy in Variable Fiber-Mat Directions Journal of Techniques Multi-Layer Woven Fiber-Mat Directions |
title | Mechanical Properties of Multi-Layer Woven E-Glass/Epoxy in Variable Fiber-Mat Directions |
title_full | Mechanical Properties of Multi-Layer Woven E-Glass/Epoxy in Variable Fiber-Mat Directions |
title_fullStr | Mechanical Properties of Multi-Layer Woven E-Glass/Epoxy in Variable Fiber-Mat Directions |
title_full_unstemmed | Mechanical Properties of Multi-Layer Woven E-Glass/Epoxy in Variable Fiber-Mat Directions |
title_short | Mechanical Properties of Multi-Layer Woven E-Glass/Epoxy in Variable Fiber-Mat Directions |
title_sort | mechanical properties of multi layer woven e glass epoxy in variable fiber mat directions |
topic | Multi-Layer Woven Fiber-Mat Directions |
url | https://journal.mtu.edu.iq/index.php/MTU/article/view/1176 |
work_keys_str_mv | AT saifaldeenghafelh mechanicalpropertiesofmultilayerwoveneglassepoxyinvariablefibermatdirections AT nasrisalhmnamer mechanicalpropertiesofmultilayerwoveneglassepoxyinvariablefibermatdirections AT abduljabbarhali mechanicalpropertiesofmultilayerwoveneglassepoxyinvariablefibermatdirections |