A Method of Structure Analysis for Complex Small HAWT Composite Blade design

碩士 === 國立虎尾科技大學 === 航空與電子科技研究所 === 101 === In order to facilitate the simulation analysis, generally the blade is simplified in flat plate shape. However, in order to conform aerodynamic efficiency, almost blade is 3D complex curved shape, therefore the existing literature is insufficient understan...

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Main Authors: Shih-Fang Wei, 魏世芳
Other Authors: 林中彥
Format: Others
Language:zh-TW
Published: 2012
Online Access:http://ndltd.ncl.edu.tw/handle/vj6u8w
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spelling ndltd-TW-101NYPI52940122019-09-22T03:41:15Z http://ndltd.ncl.edu.tw/handle/vj6u8w A Method of Structure Analysis for Complex Small HAWT Composite Blade design 小型風力機葉片之複合材料結構分析 Shih-Fang Wei 魏世芳 碩士 國立虎尾科技大學 航空與電子科技研究所 101 In order to facilitate the simulation analysis, generally the blade is simplified in flat plate shape. However, in order to conform aerodynamic efficiency, almost blade is 3D complex curved shape, therefore the existing literature is insufficient understanding of this type problems. The research applies reverse engineering method to sample the blade material in order to get the equivalent material properties of complex composite 3D blade. Analysis the blade of wind speed 8m/s、10m/s、12m/s and 25m/s pressure by the steady field, then the data input to ANSYS analysis of the displacement at one meter, finally bending test the load is requited in the same displacement. The numerical result shows there is 10.54% to 27.95% different between the experiment and FE analysis. 林中彥 2012 學位論文 ; thesis 63 zh-TW
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language zh-TW
format Others
sources NDLTD
description 碩士 === 國立虎尾科技大學 === 航空與電子科技研究所 === 101 === In order to facilitate the simulation analysis, generally the blade is simplified in flat plate shape. However, in order to conform aerodynamic efficiency, almost blade is 3D complex curved shape, therefore the existing literature is insufficient understanding of this type problems. The research applies reverse engineering method to sample the blade material in order to get the equivalent material properties of complex composite 3D blade. Analysis the blade of wind speed 8m/s、10m/s、12m/s and 25m/s pressure by the steady field, then the data input to ANSYS analysis of the displacement at one meter, finally bending test the load is requited in the same displacement. The numerical result shows there is 10.54% to 27.95% different between the experiment and FE analysis.
author2 林中彥
author_facet 林中彥
Shih-Fang Wei
魏世芳
author Shih-Fang Wei
魏世芳
spellingShingle Shih-Fang Wei
魏世芳
A Method of Structure Analysis for Complex Small HAWT Composite Blade design
author_sort Shih-Fang Wei
title A Method of Structure Analysis for Complex Small HAWT Composite Blade design
title_short A Method of Structure Analysis for Complex Small HAWT Composite Blade design
title_full A Method of Structure Analysis for Complex Small HAWT Composite Blade design
title_fullStr A Method of Structure Analysis for Complex Small HAWT Composite Blade design
title_full_unstemmed A Method of Structure Analysis for Complex Small HAWT Composite Blade design
title_sort method of structure analysis for complex small hawt composite blade design
publishDate 2012
url http://ndltd.ncl.edu.tw/handle/vj6u8w
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