热-噪声载荷作用下薄壁结构非线性动态响应分析

李纪永; 李舜酩; 沙云东

热-噪声载荷作用下薄壁结构非线性动态响应分析

1.
南京航空航天大学, 南京 210016;
2.
沈阳航空航天大学, 沈阳 110136

详细信息

作者简介:
李纪永(1985-)，博士研究生，研究方向为航空发动机强度、振动、噪声，ljynav@163.com;李舜酩(联系人)，博士，教授，smli@nuaa.edu.cn

李纪永(1985-)，博士研究生，研究方向为航空发动机强度、振动、噪声，ljynav@163.com;李舜酩(联系人)，博士，教授，smli@nuaa.edu.cn

计量
- 文章访问数: 161
- HTML全文浏览量: 25
- PDF下载量: 12
- 被引次数: 0
出版历程
- 收稿日期: 2011-06-16
- 刊出日期: 2015-06-10

Analysis of Nonlinear Dynamic Response of Thin-waU Structure Under Thermo-acoustic Loading

1.
Nanjing University of Aeronautics and Astronautics, Nanjing 210016;
2.
Shenyang Aerospace University, Shenyang 110136

摘要

摘要: 研究热噪声载荷作用下薄壁结构非线性动态响应特性,分析了薄壁结构热屈曲前后模态阵型及模态频率变化。进一步计算了热-噪声载荷联合作用下薄壁结构的横向位移响应,分析薄板中点位移概率密度,指出热屈曲板在强噪声载荷作用下,可围绕着两个平衡位置振动,发生跳变响应,且其响应频率随着声压级增大而增大。最后计算横向位移功率谱密度,研究结构几何非线性对结构刚度的影响,得出由于热及噪声对结构动态响应贡献不同,其共振频率及相应的功率谱密度发生规律性变化。
- 薄壁结构 /
- 热-噪声载荷 /
- 热屈曲 /
- 跳变响应
Abstract: This paper inv Firstly, the mode shapes estigated the characteristics of structure dynamic response under thermal-acoustic loading. and modal frequencies before and after thermal buckled were analyzed. Then the thin-wall structure out-of-plane displacement response was evaluated, by analyzing displacement probability distribution func-tion(PDF), it showed that thin wall panel vibrated around two different equilibrium configuration, that is snap-through motion, and also showed that snap-through frequencies increases with the increasing of sound pressure level (SPL). Lastly, the displacement power spectrum density (PSD) is calculated to investigate the effect of geometric nonlinearity on structure stiffness. It shows that the resonant frequency and corresponding displacement PSD change with different thermal-acoustic contributions tO structure dynamic response.
- thin-wall structure /
- thermo-acoustic loading /
- thermal buckling /
- snap-through

HTML全文

参考文献(7)

[1]	Przekop A,Rizzi S A,Sweitzer K A.An Investigation of High-Cycle Fatigue Models for Metallic Structures Exhibiting Snap-Through Response[R].AIAA,2005:55～64
[2]	Ng C F,Cleveson S A.High Intensity Acoustic Tests of aThermally Stressed Aluminum Plate in TAFA[M].NASATech Memo 101552,NASA Langley Research Center,Hampton,VA,Feb,1989
[3]	Lee J.Displacement and strain statistics of thermally buckledplates[J].Journal of Aircraft,2001,32:23～31
[4]	Mei C.Three decades'interesting experience in nonlinear finiteelement formulation development and aerospace applications[A].7th International Conference on Recent Advances in Structur-al Dynamics[C],Southampton,United Kingdom,2003
[5]	徐绯,肖寿庭.Monte-carlo伪随机历程模拟在声疲劳分析中的应用-功率谱密度法[J].机械科学与技术,1997,16(1)
[6]	范绪箕.高速飞行器热结构分析与应用[M].国防工业出版社,2009
[7]	Przekop A,Rizzi S A.Dynamic snap-through response of thin-walled structures by a reduced order method[J].AIAA Journal,2006,45(10):68～75