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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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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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.
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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 |
work_keys_str_mv |
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