摘要
论述了一个用于飞机进气道出口流场动态压力畸变测试分析的高速数据采集及实时存储处理系统的研制背景、国内外情况、主要技术难题及已完成系统的组成、功能和技术性能。
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.
出处
《力学学报》
EI
CSCD
北大核心
1997年第3期336-342,共7页
Chinese Journal of Theoretical and Applied Mechanics
基金
国家自然科学基金
中国航空工业总公司经费资助
关键词
进气道
动态压力畸变
高速数据采集
航空发动机
inlet, dynamic pressure distortion, parallel computer, high speed data acquisition, real time storing and real time processing
