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塞式喷管模拟实验及数据采集系统
引用本文:戴梧叶,刘宇,程显辰.塞式喷管模拟实验及数据采集系统[J].推进技术,2000,21(4):85-88.
作者姓名:戴梧叶  刘宇  程显辰
作者单位:北京航空航天大学,宇航学院,北京100083
基金项目:国家自然科学基金资助项目! (597860 0 1 )
摘    要:为了了解塞式喷管性能,采用固体推进剂对塞式喷管单元发动机进行了模拟实验。重点介绍了塞式喷管单元发动机模拟实验的实验系统和高精度测量系统以及数据采集软件。同时,简单说明了数据处理的方法。最后给出了典型的实验结果,该结果对塞式喷管的设计、理论研究以及数值计算有重要的参考价值。

关 键 词:火箭发动机  塞式喷管  仿真试验  数据采集

Simulated tests and data acquisition system for aerospike nozzle
Dai Wuye,Liu Yu and Cheng XianChen.Simulated tests and data acquisition system for aerospike nozzle[J].Journal of Propulsion Technology,2000,21(4):85-88.
Authors:Dai Wuye  Liu Yu and Cheng XianChen
Institution:School of Astronautics,Beijing Univ of Aeronautics and Astronautics,Beijing 100083,China;School of Astronautics,Beijing Univ of Aeronautics and Astronautics,Beijing 100083,China;School of Astronautics,Beijing Univ of Aeronautics and Astronautics,Beijing 100083,China
Abstract:To find out the performance characteristic of aerospike nozzle, the simulated tests were a aerospike engine unit using solid propellant. The experimental system and data acquisition system for simulated tests of an aerospike nozzle unit including the software of the data acquisition were presented in detail. The method of data handling was also showed summarized.Typical experimental results, which can be used as a reliable basis for the design and development of advanced aerospike engines and also can be used to validate the theoretical and numerical computation, are also showed.
Keywords:Rocket engine  Plug nozzle  Simulated test  Data acquisition  Data handling
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