期刊文献+

随机振动响应峰值因子的预计理论研究 被引量:1

Theoretical Research for Predicting Crest Factor of Random Vibration Response
下载PDF
导出
摘要 简要介绍了超越概率理论、超越频次理论、损伤等效理论和功率谱密度(PSD)的时域拟合理论等4种常见的峰值因子预计理论,并基于三角级数提出了一种新的预计理论。结合试飞加速度数据样本,对比分析超越频次理论、PSD时域拟合理论和三角级数理论的预估精度。研究表明,上述4种常见的预计理论本质上属于统计学理论;PSD时域拟合理论预计的峰值因子波动较大,峰值因子与归一化次数满足高斯分布;三角级数理论的预估精度较高,但缺乏离散峰个数的合理判据。 The work aims to briefly introduce four common theories for predicting crest factor including exceeding probability theory,exceeding frequency theory,damage equivalent theory and time-domain fitting theory of power spectral density(PSD)and propose a new prediction theory based on trigonometric series.According to the acceleration data sample during flight test,exceeding frequency theory,time-domain fitting theory of PSD and trigonometric series theory were analyzed contrastively in order to evaluate their accuracy.The analysis results showed that the above four common theories belonged to statistics theory.The crest factors predicted by time-domain fitting theory of PSD fluctuated greatly and satisfied Gauss distribution as the number of normalization.The predicting accuracy of trigonometric series theory was better,but lacked reasonable criterion to determine the number of discrete peak values.
作者 张玉杰 黄超广 段丽慧 ZHANG Yu-jie;HUANG Chao-guang;DUAN Li-hui(Strength Design and Research Department,AVIC The First Aircraft Institute,Xi’an 710089,China)
出处 《装备环境工程》 CAS 2020年第9期61-65,共5页 Equipment Environmental Engineering
关键词 随机振动 峰值因子 预计理论 概率分布 三角级数 random vibration crest factor prediction theory probability distribution trigonometric series
  • 相关文献

参考文献3

二级参考文献24

  • 1Qin Shuren,Chen Zhikui,Tang Baoping,Yang Changqi,Xu Mingtao,He Hui (Test Center, Chongqing University).RESEARCH OF WAVELET TRANSFORM INSTRUMENT SYSTEM FOR SIGNAL ANALYSIS[J].Chinese Journal of Mechanical Engineering,2000,13(2):114-121. 被引量:11
  • 2[1]Loads and Requirements for Military Aircraft. the 83rd Meeting of the AGARD SMP,Sept,1996,AGARD R-815.
  • 3[2]Design Loads for Future Aircraft. RTO Applied Vehicle Technology Panel (AVT) TG024,Feb,2002,RTO-TR-045.
  • 4[3]Struck H,Perron C. Flight Loads Derived from Operational Maneuvers. 83rd Meeting of the AGARD SMP,Sept,1996,AGARD R-815.
  • 5[4]Watson G J. Eurofighter 2000 Structure Design Criteria and Design Loading Assumptions. 83rd Meeting of the AGARD SMP,Sept,1994,AGARD R-815.
  • 6[5]Gibson D H. Evolution of F-16 Loads and Requirements. 83rd Meeting of the AGARD SMP,Sept,1996,AGARD R-815.
  • 7[6]Chamis G C. Probabilistic Approach-Composite Design. 83rd Meeting of the AGARD SMP,Sept,1996,AGARD R-815.
  • 8[7]Clay L E,Short H L. Statistical Predicting Maneuver Loads from 8-channel Flight Data. NASA CR100152,1968.
  • 9许昭鑫.随机振动[M].北京:高等教育出版社,1990.
  • 10AVERILL M L,DAVID K.Simulation Modeling and Analysis[M].New York:McGraw-Hill Book Company,1982.

共引文献66

同被引文献15

引证文献1

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部