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强制偏流喷管的实验研究
引用本文:于胜春,蔡体敏,何洪庆,张兆源,王思民.强制偏流喷管的实验研究[J].推进技术,1995,16(2):17-20,49.
作者姓名:于胜春  蔡体敏  何洪庆  张兆源  王思民
作者单位:西北工业大学航天工程学院
摘    要:介绍了整体级概念及强制偏流喷管,分析了喷管内的流场与外蜀压力变化的关系。在实验参数相同的条件下进行了与普通锥形喷管的对比实验,并测定了在发机工作过程中扩散段的压力变化,结果表明,该喷管具有良好的推力性能和自动补偿外界压力变化的能力。

关 键 词:固体推进剂  火箭发动机  喷管  喷管气流  实验

AN EXPERIMENTAL RESEARCH ON FORCED DEFLECTION NOZZLES
Yu Shengchun,Cai Timin,He Hongqing,Zhang Zhaoyuan and Wang Simin.AN EXPERIMENTAL RESEARCH ON FORCED DEFLECTION NOZZLES[J].Journal of Propulsion Technology,1995,16(2):17-20,49.
Authors:Yu Shengchun  Cai Timin  He Hongqing  Zhang Zhaoyuan and Wang Simin
Abstract:The integrated stage concept(ISC) with forced deflection nozzle (FDN) is introduced first, the working process for this nozzle at different outlet pressures is analysed. The experiments include:1)The tests compared with the conventional nozzle. On the conditions of same throat areas and same exit areas, the thrusts of the two kinds of nozzles are measured, the results'that the total impulses of the two kinds of nozzles are equal approximately can confirm that the forced deflection nozzle is feasible;2) The pressure tests. Three points in the exit cone wall and one point in the plug base are taken to test the pressure variation in the working process. Through the analysis of the pressures, it is proved that the forced deflection nozzle has the ability to compensate the variation of environmental pressure automatically. At present, the tests are going on still, the numerical simulation will be carried out to get further understanding of the flowfield of the forced deflection nozzle.
Keywords:Solid propellant rocket engine  Integrated structure  unconventional nozzle  Nozzle gas flow  Experimentation
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