Oldroyd-B流体模式在吹塑成型上之應用

碩士 === 國立清華大學 === 化學工程學系 === 87 === In this study, a Galerkin finite element numerical algorithm with splitting technique is developed to simulate the blow molding process, the Oldroyd-B viscoelastic fluid model is used as the constitutive equation to describe the isothermal forming proce...

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Main Authors: Chin-Chang Chien, 簡錦昌
Other Authors: Rong-Yeu Chang
Format: Others
Language:zh-TW
Published: 1999
Online Access:http://ndltd.ncl.edu.tw/handle/95805934250179508689
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spelling ndltd-TW-087NTHU00630172016-07-11T04:13:20Z http://ndltd.ncl.edu.tw/handle/95805934250179508689 Oldroyd-B流体模式在吹塑成型上之應用 Chin-Chang Chien 簡錦昌 碩士 國立清華大學 化學工程學系 87 In this study, a Galerkin finite element numerical algorithm with splitting technique is developed to simulate the blow molding process, the Oldroyd-B viscoelastic fluid model is used as the constitutive equation to describe the isothermal forming process of homogeneous and incompressible plastic preform. It is implemented to predict the velocity profile, pressure field, stress and part thickness distribution. Mold contact problem will be discussed after that. The results will compare with the experimental data to ensure the finally solutions.Compare the simulation results with the experimental data, preform blow pressure can be exactly predicted. The material characteristic relaxation parameter has enormously affected on the stretch in axial direction, but less affected in axial direction. As the relaxation parameter increase from 0.1 to 0.5, the stretch amount in axial direction increase one times. But as it increase from 0.5 to 2.5, the stretch amount in axial direction increase less than 0.2 times. The reason for this phenomena maybe the strain-hardening effects. Based on the simulation results, the larger the relaxation parameter, the lower needed blown pressure, and can get longer part. From the part thickness distribution, we can find it is difficult to attain part average thickness. We also know that, the inertia effects in the blow molding process simulation can be neglected because its large viscosity. Rong-Yeu Chang 張榮語 1999 學位論文 ; thesis 82 zh-TW
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language zh-TW
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sources NDLTD
description 碩士 === 國立清華大學 === 化學工程學系 === 87 === In this study, a Galerkin finite element numerical algorithm with splitting technique is developed to simulate the blow molding process, the Oldroyd-B viscoelastic fluid model is used as the constitutive equation to describe the isothermal forming process of homogeneous and incompressible plastic preform. It is implemented to predict the velocity profile, pressure field, stress and part thickness distribution. Mold contact problem will be discussed after that. The results will compare with the experimental data to ensure the finally solutions.Compare the simulation results with the experimental data, preform blow pressure can be exactly predicted. The material characteristic relaxation parameter has enormously affected on the stretch in axial direction, but less affected in axial direction. As the relaxation parameter increase from 0.1 to 0.5, the stretch amount in axial direction increase one times. But as it increase from 0.5 to 2.5, the stretch amount in axial direction increase less than 0.2 times. The reason for this phenomena maybe the strain-hardening effects. Based on the simulation results, the larger the relaxation parameter, the lower needed blown pressure, and can get longer part. From the part thickness distribution, we can find it is difficult to attain part average thickness. We also know that, the inertia effects in the blow molding process simulation can be neglected because its large viscosity.
author2 Rong-Yeu Chang
author_facet Rong-Yeu Chang
Chin-Chang Chien
簡錦昌
author Chin-Chang Chien
簡錦昌
spellingShingle Chin-Chang Chien
簡錦昌
Oldroyd-B流体模式在吹塑成型上之應用
author_sort Chin-Chang Chien
title Oldroyd-B流体模式在吹塑成型上之應用
title_short Oldroyd-B流体模式在吹塑成型上之應用
title_full Oldroyd-B流体模式在吹塑成型上之應用
title_fullStr Oldroyd-B流体模式在吹塑成型上之應用
title_full_unstemmed Oldroyd-B流体模式在吹塑成型上之應用
title_sort oldroyd-b流体模式在吹塑成型上之應用
publishDate 1999
url http://ndltd.ncl.edu.tw/handle/95805934250179508689
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