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塞式喷管气动特性与性能研究
引用本文:王长辉,刘宇,廖云飞.塞式喷管气动特性与性能研究[J].中国航空学报,2006,19(1):1-9.
作者姓名:王长辉  刘宇  廖云飞
作者单位:School of Astronautics, Beijing University of Aeronautics and Astronautics, Beijing 100083, China
摘    要:对6单元瓦状塞式喷管、6单元圆转方内喷管塞式喷管和1单元直排塞式喷管进行了实验和数值模拟研究.实验表明,3个塞式喷管具有良好的高度补偿特性和较高的效率,6单元瓦状塞式喷管和1单元直排塞式喷管在设计高度的效率接近100%;由于内喷管型面不够理想和加工时存在的缺陷,6单元圆转方内喷管塞式喷管的设计点效率在95%左右.数值模拟结果与实验数据吻合较好,结合实验和数值模拟分析了外界反压对气流,进而对底部气动特性的影响.实验研究了底部二次流流量变化对性能的影响.

关 键 词:火箭发动机  塞式喷管  性能  实验  数值模拟  rocket  engine  aerospike  nozzle  performance  experiment  numerical  simulation
文章编号:1000-9361(2006)01-0001-09
收稿时间:2005-03-19
修稿时间:2005-11-01

Studies on Aerodynamic Behavior and Performance of Aerospike Nozzles
WANG Chang-hui,LIU Yu,LIAO Yun-fei.Studies on Aerodynamic Behavior and Performance of Aerospike Nozzles[J].Chinese Journal of Aeronautics,2006,19(1):1-9.
Authors:WANG Chang-hui  LIU Yu  LIAO Yun-fei
Institution:School of Astronautics, Beijing University of Aeronautics and Astronautics, Beijing 100083, China
Abstract:Experimental and numerical studies are carried out on a 6-cell tile-shaped aerospike nozzle, a 6-cell aerospike nozzle with round-to-rectangle primary nozzles and a 1-cell linear aerospike nozzle. Good altitude compensation capacities and high efficiencies are obtained in the tests. The efficiencies of 6-cell tile-shaped aerospike nozzle and 1-cell linear aerospike nozzle at design altitude approach to 100 %, and that of 6-cell aerospike nozzle with round-to-rectangle primary nozzles in the same condition is about 95 % due to the imperfect cell contour and manufacturing defects. Numerical results are in good agreements with test data. The effects of ambient pressure on exhaust and then on base behavior are analyzed, The effects of variation in the amount of base bleed on performance are also examined in the tests.
Keywords:rocket engine  aerospike nozzle  performance  experiment  numerical simulation
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