摘要
介绍了针对航空发动机矢量喷管研究课题,开发的一套独立通讯显示系统。该系统很好地完成了矢量喷管的数模仿真、半物理模拟试验及台架试车。具有较好的可移植性和较高的工程应用价值。
This paper describes a separated communicative indication system developed for aeroengine vectoring exhaust nozzle research. Digital model simulation, semi - physical simulation tests and bench tests have been completed successfully with the system. It can be transformed easily and is valuable in engineering application.
出处
《燃气涡轮试验与研究》
2001年第2期38-41,共4页
Gas Turbine Experiment and Research