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支撑角对低冲击分离装置分离过程影响动力学仿真
引用本文:张雪原,唐文彦.支撑角对低冲击分离装置分离过程影响动力学仿真[J].固体火箭技术,2009,32(1).
作者姓名:张雪原  唐文彦
作者单位:哈尔滨工业大学,自动化测试与控制系,哈尔滨,150001
摘    要:介绍了一种低冲击分离装置的结构,并对其冷气驱动分离试验进行了分析.依据能量守恒定律和空气动力学原理,为分离装置的冷气驱动分离过程构建了数学模型;借助数学模型,对分离装置中扇形块两端的支撑角对分离过程的影响进行了仿真和分析.通过仿真结果可发现,扇形块顶端支撑角的变化对分离过程中分离时间和峰值气压的影响很小,而扇形块底端支撑角的改变则会引起分离时间和峰值气压的明显变化.因此,在保证分离功能可靠实现的前提下,可通过减小扇形块底端支撑角来降低分离过程的冲击响应.该结论对分离装置的设计和优化具有指导意义.

关 键 词:低冲击分离装置  冷气驱动试验  数学模型  仿真

Influence of support angle on air-driven separation process of low-shock separation device
ZHANG Xue-yuan,TANG Wen-yan.Influence of support angle on air-driven separation process of low-shock separation device[J].Journal of Solid Rocket Technology,2009,32(1).
Authors:ZHANG Xue-yuan  TANG Wen-yan
Institution:Automatic Measurement and Control;Harbin Institute of Technology;Harbin 15000;China
Abstract:The structure and the bench test process of a kind of low-shock separation device were introduced.According to the law of conservation of energy and aerodynamics principle,a mathematical model was established.The influence of the support angle on the air-driven separation process was simulated.The simulation results show that the change of upper support angle has little influence on the separation time and peak pressure,while the influence on the separation time and peak pressure induced by the change of lo...
Keywords:low-shock separation device  bench test  mathematical model  simulation  
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