Adaptive finite element method and its application to CFD

碩士 === 國立臺灣科技大學 === 機械工程研究所 === 83 === The aerodynamic characteristics of high speed flying vehicles are affected by many complex flow phenomena such as shock waves, boundary layer separation, vortex shedding, turbulence, etc. In recent yea...

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Main Authors: Wang Shi Jung, 王希勇
Other Authors: CyhungYuan Huang
Format: Others
Language:zh-TW
Published: 1995
Online Access:http://ndltd.ncl.edu.tw/handle/83045861133851624620
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spelling ndltd-TW-083NTUST4890402016-07-15T04:12:45Z http://ndltd.ncl.edu.tw/handle/83045861133851624620 Adaptive finite element method and its application to CFD 適應性有限元素法及其在計算流力上之應用 Wang Shi Jung 王希勇 碩士 國立臺灣科技大學 機械工程研究所 83 The aerodynamic characteristics of high speed flying vehicles are affected by many complex flow phenomena such as shock waves, boundary layer separation, vortex shedding, turbulence, etc. In recent years, the revolutionary progress of computational mechanics and the rapid development of computer hardware/ software provide an optimistic future for the realistic numerical simulation of these flow phenomena. The purpose of this study is to apply the recently developed h- adaptive finite elemen method to analyze inviscid, high speed, axisymmetric flow problems. The adaptive procedures make use of mathematically justified error indicator to evaluate the "goodness" of the numerical solution and they subsequently optimize the structure of the grid to deliver answers which satisfy user-specified levels of accuracy. The computational grid is adapted in order to reduce the error using a minimal number of degrees of freedom; this is achieved by employing nested local refinements (unrefinements) in regions of large (small) error. This type of grid-solution adaptive scheme automatically resolve shocks to a level of accuracy specified by the user and it employs minimal computational effort to achieve this task. The technical bottlenecks for implementing h- adaptive finite element method are : the treatment of constrained nodes and the design of associated data structures. In this study, a robust data structures are designed for efficiently implementing grid refinement and unrefinement. By modifying the local shape functions and the associated physical degrees of freedom in an element, the constrained nodes can be completely removed. To verify the proposed method, a series of high speed flow problems are solved and compared with either analytical solution or experimental data. The test results demonstrate that the accuracy of the numerical solution can be significantly improved by using the h-adaptive finite element method. CyhungYuan Huang 黃中元 1995 學位論文 ; thesis 87 zh-TW
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description 碩士 === 國立臺灣科技大學 === 機械工程研究所 === 83 === The aerodynamic characteristics of high speed flying vehicles are affected by many complex flow phenomena such as shock waves, boundary layer separation, vortex shedding, turbulence, etc. In recent years, the revolutionary progress of computational mechanics and the rapid development of computer hardware/ software provide an optimistic future for the realistic numerical simulation of these flow phenomena. The purpose of this study is to apply the recently developed h- adaptive finite elemen method to analyze inviscid, high speed, axisymmetric flow problems. The adaptive procedures make use of mathematically justified error indicator to evaluate the "goodness" of the numerical solution and they subsequently optimize the structure of the grid to deliver answers which satisfy user-specified levels of accuracy. The computational grid is adapted in order to reduce the error using a minimal number of degrees of freedom; this is achieved by employing nested local refinements (unrefinements) in regions of large (small) error. This type of grid-solution adaptive scheme automatically resolve shocks to a level of accuracy specified by the user and it employs minimal computational effort to achieve this task. The technical bottlenecks for implementing h- adaptive finite element method are : the treatment of constrained nodes and the design of associated data structures. In this study, a robust data structures are designed for efficiently implementing grid refinement and unrefinement. By modifying the local shape functions and the associated physical degrees of freedom in an element, the constrained nodes can be completely removed. To verify the proposed method, a series of high speed flow problems are solved and compared with either analytical solution or experimental data. The test results demonstrate that the accuracy of the numerical solution can be significantly improved by using the h-adaptive finite element method.
author2 CyhungYuan Huang
author_facet CyhungYuan Huang
Wang Shi Jung
王希勇
author Wang Shi Jung
王希勇
spellingShingle Wang Shi Jung
王希勇
Adaptive finite element method and its application to CFD
author_sort Wang Shi Jung
title Adaptive finite element method and its application to CFD
title_short Adaptive finite element method and its application to CFD
title_full Adaptive finite element method and its application to CFD
title_fullStr Adaptive finite element method and its application to CFD
title_full_unstemmed Adaptive finite element method and its application to CFD
title_sort adaptive finite element method and its application to cfd
publishDate 1995
url http://ndltd.ncl.edu.tw/handle/83045861133851624620
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