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宁交贤, 宁烽, 黄爽, 胡同, 宋志安. 飞机进气道流场压力畸变数据采集与处理系统[J]. 力学学报, 1997, 29(3): 336-342. DOI: 10.6052/0459-1879-1997-3-1995-234
引用本文: 宁交贤, 宁烽, 黄爽, 胡同, 宋志安. 飞机进气道流场压力畸变数据采集与处理系统[J]. 力学学报, 1997, 29(3): 336-342. DOI: 10.6052/0459-1879-1997-3-1995-234
DATA ACQUISITION AND PROCESSING SYSTEM USED FOR FLOW FIELD DISTORTION OF AIRCRAFT INLET[J]. Chinese Journal of Theoretical and Applied Mechanics, 1997, 29(3): 336-342. DOI: 10.6052/0459-1879-1997-3-1995-234
Citation: DATA ACQUISITION AND PROCESSING SYSTEM USED FOR FLOW FIELD DISTORTION OF AIRCRAFT INLET[J]. Chinese Journal of Theoretical and Applied Mechanics, 1997, 29(3): 336-342. DOI: 10.6052/0459-1879-1997-3-1995-234

飞机进气道流场压力畸变数据采集与处理系统

DATA ACQUISITION AND PROCESSING SYSTEM USED FOR FLOW FIELD DISTORTION OF AIRCRAFT INLET

  • 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,列出了研制中涉及到的若干关键技术

     

    Abstract: 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

     

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