Analysis of the Flexural Behavior of Laminated Plain Woven Fabric Composite C-Beams with Various Cross-Sections

碩士 === 逢甲大學 === 紡織工程學系 === 88 === In this study, carbon fiber plain woven fabrics were laminated to produce C-beam perform with various cross-sections. The Resin Transfer Molding technique was used to transfer resin into the mold by pressure difference. After the appropriate curing proces...

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Main Authors: Lai Wen Na, 賴文娜
Other Authors: Lee Wei Pin
Format: Others
Language:zh-TW
Published: 2000
Online Access:http://ndltd.ncl.edu.tw/handle/31698240861704473006
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spelling ndltd-TW-088FCU002920212015-10-13T11:53:31Z http://ndltd.ncl.edu.tw/handle/31698240861704473006 Analysis of the Flexural Behavior of Laminated Plain Woven Fabric Composite C-Beams with Various Cross-Sections 不同截面形狀之碳纖維梭織物疊層複合材料C型樑的撓曲行為分析 Lai Wen Na 賴文娜 碩士 逢甲大學 紡織工程學系 88 In this study, carbon fiber plain woven fabrics were laminated to produce C-beam perform with various cross-sections. The Resin Transfer Molding technique was used to transfer resin into the mold by pressure difference. After the appropriate curing processes, the laminated plain woven composite C-beam was produced. Three point bending test was then employed. The load-deflection curve and fracture surface were investigated. The results of the experiments showed that the flexural rigidity and the peak load increased with the web height or flange width of the specimen. For the same thickness of 2 mm, the specific flexural rigidity of the beam reaches its maximum, when the web height is approximately 5 cm , and the flange width is approximately 1 cm. The specific flexural load of the beam reaches its maximum, when the web height is approximately 3 cm and the flange width is approximately 1 cm. Therefore, we get an optimal cross-section of C-beam from experiments. From the experiments, the higher web specimen, the higher stress can be found on upper flange. Under the loading head, the sudden loss of stiffness was the result of the rupture of the material at the corners of the beam cross-section. This local loss of stiffness consequently changed the deflected shape and introduced torsion in the material underneath the loading head. For the specimen with lower web height, high stress can be found on the upper and lower flanges. The phenomenon was caused by the resin breakage. The A. Rothwell’s efficiency formulae was used to analyze for the C-beams of various cross-sections. Comparison of A.Rothwell formulae and experimental data showed that the web height of 1 cm has better accuracy. But the higher web was, the less accuracy of the analysis was. This may arise due to unwanted deformations of the beam as a result of bending-torsion and lateral buckling. Lee Wei Pin 李維平 2000 學位論文 ; thesis 70 zh-TW
collection NDLTD
language zh-TW
format Others
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description 碩士 === 逢甲大學 === 紡織工程學系 === 88 === In this study, carbon fiber plain woven fabrics were laminated to produce C-beam perform with various cross-sections. The Resin Transfer Molding technique was used to transfer resin into the mold by pressure difference. After the appropriate curing processes, the laminated plain woven composite C-beam was produced. Three point bending test was then employed. The load-deflection curve and fracture surface were investigated. The results of the experiments showed that the flexural rigidity and the peak load increased with the web height or flange width of the specimen. For the same thickness of 2 mm, the specific flexural rigidity of the beam reaches its maximum, when the web height is approximately 5 cm , and the flange width is approximately 1 cm. The specific flexural load of the beam reaches its maximum, when the web height is approximately 3 cm and the flange width is approximately 1 cm. Therefore, we get an optimal cross-section of C-beam from experiments. From the experiments, the higher web specimen, the higher stress can be found on upper flange. Under the loading head, the sudden loss of stiffness was the result of the rupture of the material at the corners of the beam cross-section. This local loss of stiffness consequently changed the deflected shape and introduced torsion in the material underneath the loading head. For the specimen with lower web height, high stress can be found on the upper and lower flanges. The phenomenon was caused by the resin breakage. The A. Rothwell’s efficiency formulae was used to analyze for the C-beams of various cross-sections. Comparison of A.Rothwell formulae and experimental data showed that the web height of 1 cm has better accuracy. But the higher web was, the less accuracy of the analysis was. This may arise due to unwanted deformations of the beam as a result of bending-torsion and lateral buckling.
author2 Lee Wei Pin
author_facet Lee Wei Pin
Lai Wen Na
賴文娜
author Lai Wen Na
賴文娜
spellingShingle Lai Wen Na
賴文娜
Analysis of the Flexural Behavior of Laminated Plain Woven Fabric Composite C-Beams with Various Cross-Sections
author_sort Lai Wen Na
title Analysis of the Flexural Behavior of Laminated Plain Woven Fabric Composite C-Beams with Various Cross-Sections
title_short Analysis of the Flexural Behavior of Laminated Plain Woven Fabric Composite C-Beams with Various Cross-Sections
title_full Analysis of the Flexural Behavior of Laminated Plain Woven Fabric Composite C-Beams with Various Cross-Sections
title_fullStr Analysis of the Flexural Behavior of Laminated Plain Woven Fabric Composite C-Beams with Various Cross-Sections
title_full_unstemmed Analysis of the Flexural Behavior of Laminated Plain Woven Fabric Composite C-Beams with Various Cross-Sections
title_sort analysis of the flexural behavior of laminated plain woven fabric composite c-beams with various cross-sections
publishDate 2000
url http://ndltd.ncl.edu.tw/handle/31698240861704473006
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