首页> 外文会议>Conference on Sensors and Smart Structures Technologies for Civil, Mechanical, and Aerospace Systems >Flutter Boundary Prediction under Continuous Variable Speed Based on Time Series Models
【24h】

Flutter Boundary Prediction under Continuous Variable Speed Based on Time Series Models

机译:基于时间序列模型的连续变速颤振边界预测

获取原文

摘要

Based on the time series model, the modal parameters of the continuous variable flutter test response signal are identified, and a set of flutter boundary prediction methods suitable for turbulent excitation is developed in this paper. In order to ensure the accuracy of the method, a modal parameter identification method is used to analyze the traditional autoregressive model (AR) and the time-varying autoregressive model (TVAR), and compare the accuracy of the two models. Finally, the method is applied to the flutter boundary prediction of turbulence signals. The prediction method combines the time series model with the stability criterion, constructs the stability parameters of the response signal, and the prediction results of flutter critical velocity are obtained by fitting and extrapolation. The numerical example shows the analysis results of the two models and proves the feasibility and effectiveness of the method. Finally, this method is used to predict the flutter boundary of low-speed wind tunnel test data, and the prediction error is less than 5%.
机译:基于时间序列模型,识别连续变量颤动试验响应信号的模态参数,并在本文中开发了一组适用于湍流激励的颤振预测方法。为了确保该方法的准确性,模态参数识别方法用于分析传统的自回归模型(AR)和时变自自回归模型(TVAR),并比较两种模型的准确性。最后,该方法应用于湍流信号的颤振边界预测。预测方法将时间序列模型与稳定性标准组合,构造响应信号的稳定性参数,并且通过拟合和外推获得颤动临界速度的预测结果。数值示例显示了两种模型的分析结果,并证明了该方法的可行性和有效性。最后,该方法用于预测低速风洞测试数据的颤振边界,并且预测误差小于5%。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号