航空学报 > 2010, Vol. 31 Issue (9): 1788-1795

不确定性颤振风险定量分析

戴玉婷, 吴志刚, 杨超   

  1. 北京航空航天大学 航空科学与工程学院
  • 收稿日期:2009-10-05 修回日期:2010-03-03 出版日期:2010-09-25 发布日期:2010-09-25
  • 通讯作者: 杨超

Quantification Analysis of Uncertain Flutter Risks

Dai Yuting, Wu Zhigang, Yang Chao   

  1. School of Aeronautic Science and Engineering, Beijing University of Aeronautics and Astronautics
  • Received:2009-10-05 Revised:2010-03-03 Online:2010-09-25 Published:2010-09-25
  • Contact: Yang Chao

摘要: 针对小风险颤振定量分析,提出一种概率鲁棒颤振初步分析方法。该方法结合鲁棒颤振分析和概率颤振分析,针对不同层次风险和不确定性水平提供颤振边界特性全面信息,给决策制定提供更好参考。在鲁棒颤振分析中,采用振型迭代的方法,通过结构奇异值( μ )分析和特征值求解得到零风险的鲁棒颤振临界速度。在概率颤振分析中,采用标准蒙特卡罗模拟(MCS)方法得到较大风险时的颤振速度分布和概率临界速度。采用概率比较和二分法估计概率鲁棒颤振不确定度半径和概率鲁棒颤振临界速度,同时采用样本重新利用的随机方法估计颤振风险和不确定性定量关系。通过一个考虑集中质量不确定性的大展弦比双梁式机翼的颤振计算分析表明,确定型μ方法只能用于零风险颤振分析,标准的MCS方法只能用于较大风险颤振速度分布问题。概率鲁棒颤振分析结果表明增加1%颤振风险可以使不确定度半径增大62%或颤振速度边界增大5%,从而放宽了设计要求。

关键词: 颤振, 概率鲁棒, 风险, 结构奇异值μ, 振型不确定性, 概率, 蒙特卡罗方法

Abstract: This article presents a preliminary method of probabilistic robust flutter analysis subject to small flutter risks. This method incorporates robust flutter analysis and probabilistic flutter analysis and is able to provide comprehensive insight into the flutter margin for different levels of risk and uncertainty to support more reasonable decision-making. In robust flutter analysis, the robust critical flutter velocity with zero risk is obtained by the structured singular value (μ) analysis and eigenvalue solution based on the modal iterative method. The probabilistic distribution of flutter velocity and probabilistic critical velocity are estimated by the standard Monte Carlo simulation (MCS) method in probabilistic flutter analysis for large risks. Probability comparison and bisection algorithm are applied to calculate the uncertainty radius and critical velocity of probabilistic robust flutter. The stochastic method with the sample reuse algorithm is also performed to obtain the quantitative relation of risk and uncertainty radius. By considering the mass uncertainty, the above methods are employed to the flutter analysis of a large aspect ratio wing with two spars. The results demonstrate that the deterministic μ method can only be used to zero risk flutter analysis while the standard MCS method is suitable just for large risk flutter analysis. The results of the probabilistic robust flutter analysis show that with 1% increment of flutter risk, the uncertainty radius can be increased by 62% or the flutter velocity can be increased by 5%. Therefore, the design requirement can be adjusted accordingly.

Key words: flutter, probabilistic robust, risk, structured singular value μ, modal uncertainty, probability, Monte Carlo method

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