%0 Journal Article %T A Real time Data Acquisition and Processing Technique for Measuring the Synthetic Pressure Distortion Parameter W in Aircraft Engine Inlet Flow
飞机发动机进口流场综合压力畸变指数W的实时采集处理软件实现技术 %A ZHAN Zhihong %A NING Jiaoxian %A
展之宏 %A 宁交贤 %J 实验力学 %D 1999 %I %X A measurement system used for acquisition and processing of pressure distortion data in aircraft engine inlet flow is briefly presented. The software realization of the system and some key techniques concerned are mainly discussed. In the system, long time data storage is realized by using an expanded memory. Some measuring results given by the system are shown. %K real %K time measuring system %K pressure distortion %K inlet flow of aircraft engin %K expanded memory %K long %K time lage capacity storage
实时处理系统 %K 压力畸变 %K 飞机发动机进口流场 %K 扩展内存 %K 大容量数据长时间存储 %U http://www.alljournals.cn/get_abstract_url.aspx?pcid=6E709DC38FA1D09A4B578DD0906875B5B44D4D294832BB8E&cid=5D344E2AD54D14F8&jid=49067A0A0D864088C06A84AACB51A5B2&aid=1A919CF32DD12222D8165020981F1FB1&yid=B914830F5B1D1078&vid=F3583C8E78166B9E&iid=0B39A22176CE99FB&sid=C5F8B8CB20F1B3D8&eid=5BC9492E1D772407&journal_id=1001-4888&journal_name=实验力学&referenced_num=1&reference_num=5