%0 Journal Article
%T DATA ACQUISITION AND PROCESSING SYSTEM USED FOR FLOW FIELD DISTORTION OF AIRCRAFT INLET<br>飞机进气道流场压力畸变数据采集与处理系统
%A Ning Jiaoxian
%A Ning Feng
%A Huang Shuang
%A <br>宁交贤
%A 宁烽
%A 黄爽
%A 胡同
%A 宋志安
%J 力学学报
%D 1997
%I 
%X This article describes a high speed data acquisition and real time storing, real time processing system for flow field distortion measurement and analysis of aircrafts' inlet/engine, focuses on system's research background, domestic and foreign information, main technical difficulties,the constitution, functions and technical properties of this completed system, finally, lists several important and key technologies solved in the period of research and manufacturing.
%K inlet
%K dynamic pressure distortion
%K parallel computer
%K high speed data acquisition
%K real
%K time storing and real
%K time processing<br>进气道
%K 动态压力畸变
%K 高速数据采集
%K 航空发动机
%U http://www.alljournals.cn/get_abstract_url.aspx?pcid=6E709DC38FA1D09A4B578DD0906875B5B44D4D294832BB8E&cid=5D344E2AD54D14F8&jid=4100DA4A1A3BA1B0CE5AD99AE1DFB420&aid=AE6D6FBC5E5081AC03086F25DE4F990E&yid=5370399DC954B911&vid=771469D9D58C34FF&iid=38B194292C032A66&sid=50EA2A80A7D254EF&eid=556C1A86E372B606&journal_id=0459-1879&journal_name=力学学报&referenced_num=1&reference_num=3