Physical, thermal, and mechanical properties of Al2O3/SiO2 infused jute/glass fiber resin composite materials in relation to viscosity

Jute/glass fibers epoxy composites are significantly used in construction, automotive, aerospace, and wind turbine industries. In this work, jute/glass fibers epoxy composites reinforced with two different types of filler such as the Al2O3 and SiO2 particles at different weight rations (5, 10, and 1...

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Veröffentlicht in:Polymer composites 2022-06, Vol.43 (6), p.3971-3982
Hauptverfasser: Shamim Hasan, Abu Hena Md, Chowdhury, Mohammad Asaduzzaman, Almahri, Albandary, Kowser, Md. Arefin, Alam, Md. Shahinoor, Shuvho, Md. Bengir Ahmed, Alruwais, Raja Saad, Hossain, Nayem, Rahman, Md. Rezaur, Rahman, Mohammed M.
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container_end_page 3982
container_issue 6
container_start_page 3971
container_title Polymer composites
container_volume 43
creator Shamim Hasan, Abu Hena Md
Chowdhury, Mohammad Asaduzzaman
Almahri, Albandary
Kowser, Md. Arefin
Alam, Md. Shahinoor
Shuvho, Md. Bengir Ahmed
Alruwais, Raja Saad
Hossain, Nayem
Rahman, Md. Rezaur
Rahman, Mohammed M.
description Jute/glass fibers epoxy composites are significantly used in construction, automotive, aerospace, and wind turbine industries. In this work, jute/glass fibers epoxy composites reinforced with two different types of filler such as the Al2O3 and SiO2 particles at different weight rations (5, 10, and 15 gm) were investigated in relation to the viscosity. The composite samples required for various tests were fabricated in conventional hand lay‐up method. Physical, thermal stability, and mechanical properties such as tensile, bending and modulus of elasticity, and viscosity tests were conducted for the fabricated composites and the effect of reinforced materials and their dispersion competency was investigated through the assessment of their microstructure with SEM, XRD, FTIR, UV, and TGA/DSC. From the results, fabricated composites exhibit linear behavior and the maximum tensile strength were found 113.438 MPa for S2 without inclusion of particles and S4 with inclusion of Al2O3 and SiO2 exhibited higher elongation 12.06%. The viscosity of the epoxy matrix showed that viscosity is increased significantly as the inclusion of the Al2O3 and SiO2 particles volume are increased. The principal weight loss takes place at 336 to 338°C, which associated weight losses were 76% for S3, 68% for S4, and 67% for S6. Jute agglomerated orientation, some void, fracture behavior, and crack have been identified, caused by lack of fiber/matrix adhesion. FTIR results show that N‐H, asymmetric stretching Si‐O‐Si, Si‐O‐C and Si‐OH bonds, C‐C stretches, C‐O bond and Al‐O‐H symmetric bonding were identified. UV analysis identified different peaks which are 254.42, 329.06, 413.5, and 473.73 nm.
doi_str_mv 10.1002/pc.26671
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Physical, thermal stability, and mechanical properties such as tensile, bending and modulus of elasticity, and viscosity tests were conducted for the fabricated composites and the effect of reinforced materials and their dispersion competency was investigated through the assessment of their microstructure with SEM, XRD, FTIR, UV, and TGA/DSC. From the results, fabricated composites exhibit linear behavior and the maximum tensile strength were found 113.438 MPa for S2 without inclusion of particles and S4 with inclusion of Al2O3 and SiO2 exhibited higher elongation 12.06%. The viscosity of the epoxy matrix showed that viscosity is increased significantly as the inclusion of the Al2O3 and SiO2 particles volume are increased. The principal weight loss takes place at 336 to 338°C, which associated weight losses were 76% for S3, 68% for S4, and 67% for S6. Jute agglomerated orientation, some void, fracture behavior, and crack have been identified, caused by lack of fiber/matrix adhesion. FTIR results show that N‐H, asymmetric stretching Si‐O‐Si, Si‐O‐C and Si‐OH bonds, C‐C stretches, C‐O bond and Al‐O‐H symmetric bonding were identified. 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Physical, thermal stability, and mechanical properties such as tensile, bending and modulus of elasticity, and viscosity tests were conducted for the fabricated composites and the effect of reinforced materials and their dispersion competency was investigated through the assessment of their microstructure with SEM, XRD, FTIR, UV, and TGA/DSC. From the results, fabricated composites exhibit linear behavior and the maximum tensile strength were found 113.438 MPa for S2 without inclusion of particles and S4 with inclusion of Al2O3 and SiO2 exhibited higher elongation 12.06%. The viscosity of the epoxy matrix showed that viscosity is increased significantly as the inclusion of the Al2O3 and SiO2 particles volume are increased. The principal weight loss takes place at 336 to 338°C, which associated weight losses were 76% for S3, 68% for S4, and 67% for S6. Jute agglomerated orientation, some void, fracture behavior, and crack have been identified, caused by lack of fiber/matrix adhesion. FTIR results show that N‐H, asymmetric stretching Si‐O‐Si, Si‐O‐C and Si‐OH bonds, C‐C stretches, C‐O bond and Al‐O‐H symmetric bonding were identified. UV analysis identified different peaks which are 254.42, 329.06, 413.5, and 473.73 nm.</description><subject>Aerospace industry</subject><subject>Aluminum oxide</subject><subject>Automotive glass</subject><subject>Composite materials</subject><subject>composites</subject><subject>Elongation</subject><subject>Fiber-matrix adhesion</subject><subject>filler materials</subject><subject>Glass fiber reinforced plastics</subject><subject>Glass-epoxy composites</subject><subject>Jute</subject><subject>jute/glass fibers</subject><subject>Mechanical properties</subject><subject>Modulus of elasticity</subject><subject>morphology</subject><subject>Polymer matrix composites</subject><subject>Silicon dioxide</subject><subject>Tensile strength</subject><subject>Thermal stability</subject><subject>Viscosity</subject><subject>Weight loss</subject><subject>Wind turbines</subject><issn>0272-8397</issn><issn>1548-0569</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2022</creationdate><recordtype>article</recordtype><recordid>eNotkFtLwzAYhoMoOKfgTwh4a7ekSdP2cgxPMNhAvQ5p-sVl9GSSKv0D_m6z6dX7wft8pxehW0oWlJB0OehFKkROz9CMZrxISCbKczQjaZ4mBSvzS3Tl_SGSVAg2Qz-7_eStVs09Dntw7bFQXY1b0HvVHQ08uH4AFyx43Bu8atItW77abYptZ0YPNT6MAZYfjfIeG1uBww687bDu26H3NgBuVQBnVeNjSzQbFWzf4dDjL-v1EZmu0YWJPtz86xy9Pz68rZ-TzfbpZb3aJANlgiZ1qcs8Hs4rXarccG6UgpqUhTBCG8UE46QCWmsKXHCRCTCCZjojdZUDKzibo7u_ufGpzxF8kId-dF1cKVORZ5wXZUkjlfxR37aBSQ7OtspNkhJ5jFgOWp4ilrv1SdkvldlxrQ</recordid><startdate>202206</startdate><enddate>202206</enddate><creator>Shamim Hasan, Abu Hena Md</creator><creator>Chowdhury, Mohammad Asaduzzaman</creator><creator>Almahri, Albandary</creator><creator>Kowser, Md. 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Physical, thermal stability, and mechanical properties such as tensile, bending and modulus of elasticity, and viscosity tests were conducted for the fabricated composites and the effect of reinforced materials and their dispersion competency was investigated through the assessment of their microstructure with SEM, XRD, FTIR, UV, and TGA/DSC. From the results, fabricated composites exhibit linear behavior and the maximum tensile strength were found 113.438 MPa for S2 without inclusion of particles and S4 with inclusion of Al2O3 and SiO2 exhibited higher elongation 12.06%. The viscosity of the epoxy matrix showed that viscosity is increased significantly as the inclusion of the Al2O3 and SiO2 particles volume are increased. The principal weight loss takes place at 336 to 338°C, which associated weight losses were 76% for S3, 68% for S4, and 67% for S6. Jute agglomerated orientation, some void, fracture behavior, and crack have been identified, caused by lack of fiber/matrix adhesion. FTIR results show that N‐H, asymmetric stretching Si‐O‐Si, Si‐O‐C and Si‐OH bonds, C‐C stretches, C‐O bond and Al‐O‐H symmetric bonding were identified. UV analysis identified different peaks which are 254.42, 329.06, 413.5, and 473.73 nm.</abstract><cop>Hoboken, USA</cop><pub>John Wiley &amp; Sons, Inc</pub><doi>10.1002/pc.26671</doi><tpages>12</tpages><orcidid>https://orcid.org/0000-0003-2773-1244</orcidid><orcidid>https://orcid.org/0000-0002-3809-2559</orcidid></addata></record>
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source Wiley Online Library Journals Frontfile Complete
subjects Aerospace industry
Aluminum oxide
Automotive glass
Composite materials
composites
Elongation
Fiber-matrix adhesion
filler materials
Glass fiber reinforced plastics
Glass-epoxy composites
Jute
jute/glass fibers
Mechanical properties
Modulus of elasticity
morphology
Polymer matrix composites
Silicon dioxide
Tensile strength
Thermal stability
Viscosity
Weight loss
Wind turbines
title Physical, thermal, and mechanical properties of Al2O3/SiO2 infused jute/glass fiber resin composite materials in relation to viscosity
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