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脉冲爆震发动机(PDE)引射增推装置试验 被引量:3

Experimental Investigation on Thrust Augmentation of Pulsed Detonation Engine(PDE)
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摘要 PDE设计了两种结构的排气引射增推装置,通过对两种结构排气引射增推装置的试验对比,研究了排气引射增推装置对PDE推力贡献,试验结果表明在合理的结构设计下,采用排气引射增推装置可使PDE平均推力增加50%左右。理论分析了排气引射增推装置的工作机理,及不同结构参数对PDE排气引射增推装置的影响,为PDE排气引射增推装置优化设计提供了理论和试验依据。 A preliminary experimental investigation on the effect of thrust augmentation on Pulsed Detonation Engine (PDE) performance was performed. Two different thrust augmentation geometries were designed and tested. The results show that in average more than 50% thrust increment could be gained under rational construction parameters. Analysis of the mechanism of thrust augmentation and the influence of different construction parameters on thrust improve ment was performed. These results offered basic reference for design optimization of the PDE thrust augmentation.
出处 《航空动力学报》 EI CAS CSCD 北大核心 2005年第6期983-988,共6页 Journal of Aerospace Power
关键词 航空 航天推进系统 脉冲爆震发动机(PDE) 推力 排气引射增推装置 结构参数 aerospace propulsion system Pulsed Detonation Engine (PDE) thrust thrust augmentation optimized parameters
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参考文献9

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同被引文献39

  • 1郑殿峰,王家骅,王波,李建中,范育新,张会强,林文漪.脉冲爆震发动机旋流式气动阀工作机理和扰流器阻力特性的实验研究[J].南京航空航天大学学报,2005,37(1):101-105. 被引量:15
  • 2黄希桥,严传俊,范玮,王治武,郑龙席,李牧.脉冲爆震发动机引射器的实验研究[J].机械科学与技术,2005,24(8):999-1001. 被引量:3
  • 3宫翔飞,张树道,江松.界面捕捉Level Set方法的(AMR)数值模拟[J].计算物理,2006,23(4):391-395. 被引量:12
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