Study on the strength of FRP Rotor Blade and Structural Optimization
碩士 === 國立臺灣大學 === 工程科學與海洋工程學系 === 91 === Research on optimization of FRP rotor blade by the finite element method is accomplished. Utilizing ABAQUS software to model the rotor blade and analyze it by large deformation theory numerically. Optimal tool is the genetic algorithms﹙GA﹚. GA has...
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ndltd-TW-091NTU003450302016-06-20T04:15:29Z http://ndltd.ncl.edu.tw/handle/76450032470488992767 Study on the strength of FRP Rotor Blade and Structural Optimization FRP旋翼之強度分析及結構最佳化探討 Chin-Chih Chi 紀金池 碩士 國立臺灣大學 工程科學與海洋工程學系 91 Research on optimization of FRP rotor blade by the finite element method is accomplished. Utilizing ABAQUS software to model the rotor blade and analyze it by large deformation theory numerically. Optimal tool is the genetic algorithms﹙GA﹚. GA has applied to the many optimal problems by the design variables and objection function. GA searches the global optimum in the region that has many peaks by utilizing the basic operations of selection, crossover and mutate. There is twist deformation due to applying the loads to the rotor blade. The deformations make the aerodynamic force to change. There are harmful influence in design and controlling the rotor blade. FRP laminates may reinforce the structural directional stiffness to improve the drawback. The research is utilizing the material property and laminate angles of FRP laminates to obtain the smallest twist deformation. The restrictions on the optimal problem are stress failure of laminate materials, natural resonance of structure and minimum auto-rotational inertia moment. Ya-Jung Lee 李雅榮 2003 學位論文 ; thesis 67 zh-TW |
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碩士 === 國立臺灣大學 === 工程科學與海洋工程學系 === 91 === Research on optimization of FRP rotor blade by the finite element method is accomplished. Utilizing ABAQUS software to model the rotor blade and analyze it by large deformation theory numerically. Optimal tool is the genetic algorithms﹙GA﹚. GA has applied to the many optimal problems by the design variables and objection function. GA searches the global optimum in the region that has many peaks by utilizing the basic operations of selection, crossover and mutate. There is twist deformation due to applying the loads to the rotor blade. The deformations make the aerodynamic force to change. There are harmful influence in design and controlling the rotor blade. FRP laminates may reinforce the structural directional stiffness to improve the drawback. The research is utilizing the material property and laminate angles of FRP laminates to obtain the smallest twist deformation. The restrictions on the optimal problem are stress failure of laminate materials, natural resonance of structure and minimum auto-rotational inertia moment.
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Ya-Jung Lee |
author_facet |
Ya-Jung Lee Chin-Chih Chi 紀金池 |
author |
Chin-Chih Chi 紀金池 |
spellingShingle |
Chin-Chih Chi 紀金池 Study on the strength of FRP Rotor Blade and Structural Optimization |
author_sort |
Chin-Chih Chi |
title |
Study on the strength of FRP Rotor Blade and Structural Optimization |
title_short |
Study on the strength of FRP Rotor Blade and Structural Optimization |
title_full |
Study on the strength of FRP Rotor Blade and Structural Optimization |
title_fullStr |
Study on the strength of FRP Rotor Blade and Structural Optimization |
title_full_unstemmed |
Study on the strength of FRP Rotor Blade and Structural Optimization |
title_sort |
study on the strength of frp rotor blade and structural optimization |
publishDate |
2003 |
url |
http://ndltd.ncl.edu.tw/handle/76450032470488992767 |
work_keys_str_mv |
AT chinchihchi studyonthestrengthoffrprotorbladeandstructuraloptimization AT jìjīnchí studyonthestrengthoffrprotorbladeandstructuraloptimization AT chinchihchi frpxuányìzhīqiángdùfēnxījíjiégòuzuìjiāhuàtàntǎo AT jìjīnchí frpxuányìzhīqiángdùfēnxījíjiégòuzuìjiāhuàtàntǎo |
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1718310146012086272 |