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变推力发动机仿真计算分析
引用本文:唐虎,张涛,刘昌波.变推力发动机仿真计算分析[J].火箭推进,2008,34(5):1-4.
作者姓名:唐虎  张涛  刘昌波
作者单位:西安航天动力研究所,陕西,西安,710100
摘    要:分析了变推力发动机采用的双调模式,用流量调节器控制推进剂流量。流量定位针栓式喷注器控制喷注压降,保证喷注速度基本不变。根据发动机系统特点建立了主要组件的数学模型,并根据模型进行了仿真计算,最后对发动机前管路流阻影响进行了分析。

关 键 词:变推力发动机  喷注器  燃烧室

Computational analysis of a variable-thrust engine
Tang Hu,Zhang Tao,Liu Changbo.Computational analysis of a variable-thrust engine[J].Journal of Rocket Propulsion,2008,34(5):1-4.
Authors:Tang Hu  Zhang Tao  Liu Changbo
Institution:Tang Hu,Zhang Tao,Liu Changbo (Xi\'an Aerospace Propulsion Institute,Xi\'an 710100,China)
Abstract:A variable-thrust engine uses a regulator to control the flowrate and a flowrate positioned pintle injector to control the injection pressure drop, thus to maintain a stable injection velocity. In this paper, based on the characteritics of the engine system, the main components models are established and simulated. At the end, the influence of flow resistance in the pipeline upstream the engine on the engine performance is analyzed.
Keywords:variable-thrust engine  injector  combustion chamber  
本文献已被 CNKI 维普 万方数据 等数据库收录!
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