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带喷管脉冲爆震发动机单循环性能分析模型
引用本文:邱华,严传俊,熊姹.带喷管脉冲爆震发动机单循环性能分析模型[J].航空动力学报,2005,20(5):818-821.
作者姓名:邱华  严传俊  熊姹
作者单位:西北工业大学动力与能源学院,陕西西安710072
基金项目:国家自然科学基金资助(50336030),西北工业大学博士创新基金资助
摘    要:利用特征线理论下爆震波传播过程的解析解形式,采用爆震室内气体状态均一化处理方法,将爆震波到达爆震室出口或隔离气体接触面(部分充填下)以后通过收敛扩张喷管的排气过程简化为固定容积排气的零维模型,在此基础上得到了相应的性能计算模型。通过与试验数据的对比表明,模型可以有效评估喷管结构尺寸对发动机性能的影响趋势,通过引入一定的拟合形式,可以计算同一发动机结构下不同状态时的性能。 

关 键 词:航空、航天推进系统    脉冲爆震发动机    喷管    部分充填    性能模型
文章编号:1000-8055(2005)05-0818-04
收稿时间:2005/3/29 0:00:00
修稿时间:2005年3月29日

A Single-Cycle Performance Model of the Pulse Detonation Engine with Nozzle
QIU Hu,YAN Chuan-jun and XIONG Cha.A Single-Cycle Performance Model of the Pulse Detonation Engine with Nozzle[J].Journal of Aerospace Power,2005,20(5):818-821.
Authors:QIU Hu  YAN Chuan-jun and XIONG Cha
Institution:School of Power and Energy,Northwestern Polytechnical University,Xi'an710072,China
Abstract:A performance analysis model of pulse detonation engine with convergent-divergent nozzle was established.By using detonation transmission analytical solution of characteristic method and processing method of homogeneous state of detonation chamber,the exhaust process through the nozzle after the detonation wave arriving the exit of detonation chamber or the contact face of purge gas was simplified to a fixed exhaust volume zero dimensional model.Compared with the experimental data,the model developed can be used for evaluating the engine performance trend of different nozzle sizes.Through applying some curve fitting,the model can be used for calculating the engine performance at different regimes.
Keywords:aerospace propulsion system  pulse detonation engine  nozzle  partial filling  performance model
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