复合材料机翼盒段的设计、模态分析和试验

刘兵山; 燕瑛; 钱卫; 段跃新

复合材料机翼盒段的设计、模态分析和试验

1.
北京航空航天大学材料科学与工程学院, 北京 100083
2. 沈阳飞机设计研究所, 沈阳 110035

基金项目: 航空科学基金资助项目(02G51080)

详细信息

作者简介:
刘兵山(1975-),男,陕西淳化人,博士生, keasice@btamail.net.cn.

中图分类号: V 2148
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- 被引次数: 0
出版历程
- 收稿日期: 2003-06-25
- 网络出版日期: 2003-11-30

Design, modal analysis and tests of composites wing box

1.
School of Aeronautics Science and Technology, Beijing University of Aeronautics and Astronautics, Beijing 100083, China
2. Shenyang Aircraft Design Research Institute, Shenyang 110035, China

摘要

摘要: 为了进行机翼盒段结构的模态分析和试验,依据结构相似方法对盒段进行缩比,采用复合材料整体成型技术制造盒段模型,该模型同时实现了结构动力学相似与传力相似.对模型进行了模态分析和试验,两者结果吻合较好.本模型为在低速风洞中实现高速飞机机翼颤振试验奠定了基础.
- 复合材料 /
- 模态分析 /
- 制造 /
- 试验 /
- 机翼盒段
Abstract: A scaling-down wing-box model was designed on the basis of structural similarity and manufactured by means of integral-forming of composites for modal analysis and test, in which the similarity of structural dynamics and loading transfer were realized at the same time. The modal analysis and test was done and the results were in good agreement. This model lays a foundation of the flutter test of high-speed wing in low-speed wind tunnel.
- composite materials /
- modal analysis /
- manufacting /
- tests /
- wing-box

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参考文献(1)

[1] 燕瑛,黄聪,成传贤,等. 低模量复合材料刚度和强度的分析与实验研究. 见:王玉林.第12届全国复合材料会议论文集. 天津:天津大学出版社, 2002. 786~789 Yan Ying, Huang Cong, Cheng Chuanxian, et al. Analysis and experimental study of stiffness and strength of low modulus composites. In:Wang Yulin. The 12nd National Conference on Composite Materials. Tianjin:Tianjin University Press, 2002. 786~789(in Chinese) [2] Silva W A, Bartels R E. Development of reduced-order models for aeroelastic analysis and flutter prediction using the CFL3Dv6.0 code. AIAA A0228399, 2002 [3] Stroud W J, Krishnamurthy T, Mason B H, et al. Probabilistic design of a plate-like wing to meet flutter and strength requirements. AIAA A0231150, 2002 [4] Jinsoo Cho, Younhyuck Chang. Supersonic flutter analysis of wings using an unsteady 3D panel method[J]. Computers & Fluids, 2001, 30:237~256

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