| 复合材料翼面结构优化设计及分析 |
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| 引用本文： | 柴红普,于哲峰,傅山.复合材料翼面结构优化设计及分析[J].上海力学,2011,32(1):109-116. |
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| 作者姓名： | 柴红普 于哲峰 傅山 |
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| 作者单位： | 上海交通大学航空航天学院; |
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| 摘 要： | 复合材料具有比强度高、比刚度大、抗疲劳等诸多优异性能,在航空航天结构中得到了广泛的应用.复合材料在新研制的飞机上的应用比重也越来越高,在大型民用飞机Boeing787上,复合材料结构重量占到了全机结构重量的50%.复合材料层合板具有无与伦比的设计潜力,成为复合材料中使用最多的一种结构形式.本文以某型号飞机机翼翼盒为研究...
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| 关 键 词： | 复合材料 层合板 优化设计 翼盒结构 |
Optimization Design and Analysis of Composite Wing Skins |
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| CHAI Hong-pu,YU Zhe-feng,FU Shan.Optimization Design and Analysis of Composite Wing Skins[J].Chinese Quarterly Mechanics,2011,32(1):109-116. |
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| Authors: | CHAI Hong-pu YU Zhe-feng FU Shan |
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| Institution: | CHAI Hong-pu,YU Zhe-feng,FU Shan(School of Aeronautics and Astronautics,Shanghai Jiaotong University,Shanghai,200240,China) |
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| Abstract: | Composite material has been widely used in aviation and aerospace industry because of its some excellent performances such as excellent fatigue,high strength and stiffness ratio etc.Composite laminate has unmatched design potential,so it is used most among all the types of composite materials.More and more composite material is used in the new designed plane,and half of the structure weight of Boeing 787 is also composite material.In this paper,the wing box is selected as the research objective and the fini... |
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| Keywords: | composite laminate optimization design wing box |
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