| 大展弦比复合材料机翼动力学分析 |
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| 引用本文： | 王洪伟,杨茂.大展弦比复合材料机翼动力学分析[J].计算机辅助工程,2008,17(2):21-23. |
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| 作者姓名： | 王洪伟 杨茂 |
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| 作者单位： | 西北工业大学,航天学院,西安,710072 |
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| 摘 要： | 针对结构非线性对大展弦比机翼动力学特性影响很大的问题，使用MSC Patran和MSC Nastran软件进行有限元建模及分析，将大展弦比机翼建成薄壁盒型梁模型．研究大变形对机翼动力学特性的影响，比较复合材料盒型梁模型和金属盒型梁模型的计算结果，并讨论复合材料铺层顺序的改变对机翼动力学特性的影响．研究表明：复合材料机翼的各阶固有频率明显高于铝合金机翼；铺层顺序会影响复合材料机翼的固有频率．
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| 关 键 词： | 大展弦比机翼 复合材料 盒型梁 有限元 MSC Patran MSC Nastran |
| 文章编号： | 1006-0871(2008)02-0021-04 |
| 收稿时间： | 2007/6/29 0:00:00 |
| 修稿时间： | 2007年6月29日 |
Dynamic analysis on high aspect ratio composite wing |
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| WANG Hongwei and YANG Mao.Dynamic analysis on high aspect ratio composite wing[J].Computer Aided Engineering,2008,17(2):21-23. |
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| Authors: | WANG Hongwei and YANG Mao |
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| Affiliation: | WANG Hongwei,YANG Mao(School of Astronautics,Northwestern Polytechnical Univ.,Xi'an 710072,China) |
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| Abstract: | With the issue that structural nonlinearity has great effect on dynamic characteristics of high aspect ratio wing,the finite element modeling is built for high aspect ratio composite wing by using MSC Patran and Nastran,which is modeled as a thin-walled box beam.The effects of large deflections on dynamic characteristics of wing are studied.The computation results of composite box beam model are compared with metal box beam model.The effects of ply sequence of composite on dynamic characteristics are also d... |
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| Keywords: | high aspect ratio wing composite box beam finite element MSC Patran MSC Nastran |
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