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φ180mm脉冲爆震发动机热力性能研究

刘鸿 王家骅 张义宁 唐豪 张靖周

刘鸿, 王家骅, 张义宁, 唐豪, 张靖周. φ180mm脉冲爆震发动机热力性能研究[J]. 航空动力学报, 2007, 22(10): 1627-1631.
引用本文: 刘鸿, 王家骅, 张义宁, 唐豪, 张靖周. φ180mm脉冲爆震发动机热力性能研究[J]. 航空动力学报, 2007, 22(10): 1627-1631.
LIU Hong, WANG Jia-hua, ZHANG Yi-ning, TANG Hao, ZHANG Jing-zhou. Investigation on thermodynamic performance of pulse detonation engine with 180 mm[J]. Journal of Aerospace Power, 2007, 22(10): 1627-1631.
Citation: LIU Hong, WANG Jia-hua, ZHANG Yi-ning, TANG Hao, ZHANG Jing-zhou. Investigation on thermodynamic performance of pulse detonation engine with 180 mm[J]. Journal of Aerospace Power, 2007, 22(10): 1627-1631.

φ180mm脉冲爆震发动机热力性能研究

基金项目: 国防基础预研项目(A2520060227)

Investigation on thermodynamic performance of pulse detonation engine with 180 mm

  • 摘要: 采用经验数据和计算相结合的方法预估直径180 mm,长度为2.2 m带气动阀的脉冲爆震发动机(Pulse Detonation Engine,简称PDE)的性能,并考虑PDE内的总压损失.计算结果和实测结果基本吻合.计算中发现,由于考虑了PDE内总压损失,PDE推力比理想情况低,油耗比理想情况大.该计算方法对预估实际PDE工作性能具有较大的参考价值.

     

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出版历程
  • 收稿日期:  2007-02-08
  • 修回日期:  2007-07-11
  • 刊出日期:  2007-10-28

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