Numerical implementation of boundary element method for determining aerodynamic characteristics around airfoil system by viscous media

Numerical implementation of boundary element method for determining aerodynamic characteristics around airfoil system by viscous media

In this paper, the boundary element method is applied to determine the characteristics of distributed flow around the airfoil group. Because the boundary integral equation can describe various initial boundary value problems in mechanics and has many advantages such as good convergence, it can be us...

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Main Authors: Ke Xu, Peng Yue, Qiang Liu, Chuange Liu, Yiyu Lu, Jinghui Zhang
Format: Article
Language:English
Published: AIP Publishing LLC 2020-05-01
Series:AIP Advances
Online Access:http://dx.doi.org/10.1063/1.5143381
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spelling doaj-c38e34335d694ce3adfab7c62f0dc3802020-11-25T03:02:13ZengAIP Publishing LLCAIP Advances2158-32262020-05-01105055126055126-610.1063/1.5143381Numerical implementation of boundary element method for determining aerodynamic characteristics around airfoil system by viscous mediaKe Xu0Peng Yue1Qiang Liu2Chuange Liu3Yiyu Lu4Jinghui Zhang5School of Aeronautics and Astronautics, University of Electronic Science and Technology of China, Chengdu, Sichuan Province 611731, ChinaSchool of Aeronautics and Astronautics, University of Electronic Science and Technology of China, Chengdu, Sichuan Province 611731, ChinaSchool of Aeronautics and Astronautics, University of Electronic Science and Technology of China, Chengdu, Sichuan Province 611731, ChinaSchool of Aeronautics and Astronautics, University of Electronic Science and Technology of China, Chengdu, Sichuan Province 611731, ChinaSchool of Aeronautics and Astronautics, University of Electronic Science and Technology of China, Chengdu, Sichuan Province 611731, ChinaSchool of Aeronautics and Astronautics, University of Electronic Science and Technology of China, Chengdu, Sichuan Province 611731, ChinaIn this paper, the boundary element method is applied to determine the characteristics of distributed flow around the airfoil group. Because the boundary integral equation can describe various initial boundary value problems in mechanics and has many advantages such as good convergence, it can be used as a tool to establish appropriate mathematical models and numerical realization methods, so as to comprehensively study the distribution kinematics and dynamics of the airfoil group motion system in the viscous fluid flow co-flow process. In this paper, some numerical results are presented to determine the aerodynamic distribution characteristics of the viscous flow field around the airfoil group in the control area.http://dx.doi.org/10.1063/1.5143381
collection DOAJ
language English
format Article
sources DOAJ
author Ke Xu
Peng Yue
Qiang Liu
Chuange Liu
Yiyu Lu
Jinghui Zhang
spellingShingle Ke Xu
Peng Yue
Qiang Liu
Chuange Liu
Yiyu Lu
Jinghui Zhang
Numerical implementation of boundary element method for determining aerodynamic characteristics around airfoil system by viscous media
AIP Advances
author_facet Ke Xu
Peng Yue
Qiang Liu
Chuange Liu
Yiyu Lu
Jinghui Zhang
author_sort Ke Xu
title Numerical implementation of boundary element method for determining aerodynamic characteristics around airfoil system by viscous media
title_short Numerical implementation of boundary element method for determining aerodynamic characteristics around airfoil system by viscous media
title_full Numerical implementation of boundary element method for determining aerodynamic characteristics around airfoil system by viscous media
title_fullStr Numerical implementation of boundary element method for determining aerodynamic characteristics around airfoil system by viscous media
title_full_unstemmed Numerical implementation of boundary element method for determining aerodynamic characteristics around airfoil system by viscous media
title_sort numerical implementation of boundary element method for determining aerodynamic characteristics around airfoil system by viscous media
publisher AIP Publishing LLC
series AIP Advances
issn 2158-3226
publishDate 2020-05-01
description In this paper, the boundary element method is applied to determine the characteristics of distributed flow around the airfoil group. Because the boundary integral equation can describe various initial boundary value problems in mechanics and has many advantages such as good convergence, it can be used as a tool to establish appropriate mathematical models and numerical realization methods, so as to comprehensively study the distribution kinematics and dynamics of the airfoil group motion system in the viscous fluid flow co-flow process. In this paper, some numerical results are presented to determine the aerodynamic distribution characteristics of the viscous flow field around the airfoil group in the control area.
url http://dx.doi.org/10.1063/1.5143381
work_keys_str_mv AT kexu numericalimplementationofboundaryelementmethodfordeterminingaerodynamiccharacteristicsaroundairfoilsystembyviscousmedia
AT pengyue numericalimplementationofboundaryelementmethodfordeterminingaerodynamiccharacteristicsaroundairfoilsystembyviscousmedia
AT qiangliu numericalimplementationofboundaryelementmethodfordeterminingaerodynamiccharacteristicsaroundairfoilsystembyviscousmedia
AT chuangeliu numericalimplementationofboundaryelementmethodfordeterminingaerodynamiccharacteristicsaroundairfoilsystembyviscousmedia
AT yiyulu numericalimplementationofboundaryelementmethodfordeterminingaerodynamiccharacteristicsaroundairfoilsystembyviscousmedia
AT jinghuizhang numericalimplementationofboundaryelementmethodfordeterminingaerodynamiccharacteristicsaroundairfoilsystembyviscousmedia
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