首页 | 本学科首页   官方微博 | 高级检索  
     检索      

高频压力探针动态性能的补偿方法
引用本文:郭勇,王效葵,王洪伟.高频压力探针动态性能的补偿方法[J].航空动力学报,2005,20(2):273-277.
作者姓名:郭勇  王效葵  王洪伟
作者单位:北京航空航天大学,能源与动力工程学院,北京,100083
摘    要:在压气机流场的动态测试中,为了应用现有的高频压力探针测得更高频率的信号,需要展宽高频压力探针的工作频带。在对高频压力探针进行动态校准的基础上,利用动态补偿数字滤波器技术展宽高频压力探针的工作频带从而改善高频压力探针的动态特性,提高了高频压力探针的响应速度。

关 键 词:航空、航天推进系统  压气机  流场动态测试  动态性能  动态补偿数字滤波器
文章编号:1000-8055(2005)02-0273-05
收稿时间:3/9/2004 12:00:00 AM
修稿时间:2004年3月9日

Improvement on Dynamic Characteristics of High Response Pressure Probe
GUO Yong,WANG Xiao-kui and WANG Hong-wei.Improvement on Dynamic Characteristics of High Response Pressure Probe[J].Journal of Aerospace Power,2005,20(2):273-277.
Authors:GUO Yong  WANG Xiao-kui and WANG Hong-wei
Institution:School of Jet Propulsion,Beijing University of Aeronautics and Astronautics,Beijing100083,China;School of Jet Propulsion,Beijing University of Aeronautics and Astronautics,Beijing100083,China;School of Jet Propulsion,Beijing University of Aeronautics and Astronautics,Beijing100083,China
Abstract:It is necessary to broaden the working frequency band of the existing high response pressure probe to make it can be used to measure the compressor dynamic flow field.On the basis of dynamic calibration,the application of the dynamic compensation digital filter technique will improve the dynamic characteristics,and thus its response time is shortened and the frequency band is broadened.
Keywords:aerospace propulsion system  compressor  high response pressure probe  dynamic flow field  dynamic characteristics  dynamic compensation digital filter  
本文献已被 CNKI 万方数据 等数据库收录!
点击此处可从《航空动力学报》浏览原始摘要信息
点击此处可从《航空动力学报》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号