Influence of Incident Pressure on Continuous Supersonic Jet Collision

  • ZHAO Kun ,
  • DIAO Zhicheng ,
  • HE Liming ,
  • ZENG Hao ,
  • ZHANG Shengli ,
  • XIE Xiangyong
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  • 1 Aeronautics Engineering College, Air Force Engineering University, Xian 710038, China
    2 No. 95896 Unit, Hebei Cangzhou 061700, China
    3 No. 93716 Unit, Tianjin 300000, China
    4 No. 94855 Unit, Zhejiang Quzhou 324000, China

Received date: 2017-10-11

  Online published: 2025-05-29

Abstract

In order to research the influence of the free supersonic jet pressure on jet collision, taking air as media, the experiment and numerical simulation of continuous supersonic jet collision in free space under different incident pressure were carried out. and the dynamic pressure and radiation noise of the jet collision center were analyzed. The results show that the dynamic pressure amplitude and the frequency of jet collision gradually increase as the injection pressure increases. At the same time the frequency of the noise caused by jet collision increases. The increase of the incident pressure can improve the effect of jet collision.

Cite this article

ZHAO Kun , DIAO Zhicheng , HE Liming , ZENG Hao , ZHANG Shengli , XIE Xiangyong . Influence of Incident Pressure on Continuous Supersonic Jet Collision[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2018 , 38(5) : 55 -59 . DOI: 10.15892/j.cnki.djzdxb.2018.05.014

References

[1]
ROY G D, FROLOV S M, BORISOV A A, et al. Pulsed detonation propulsion: challenges,current status,and future perspective[J]. Progress in Energy and Combustion Science, 2004, 30(6): 545-672.
[2]
KHOKHLOV A M, ORAN S, THOMAS G O. Numerical simulation of deflagration-to-detonation transition: The role of shock-flame interactions in turbulent flames[J]. Combustion and Fame, 1999, 117(1/2): 323-339.
[3]
KAILASANATH K. Recet developments in the research on pulse detonation enjines[J]. AIAA Journal, 2003, 41(2): 145-159.
[4]
何立明, 荣康, 曾昊, 等. 激波聚焦及起爆爆震波的研究进展[J]. 推进技术, 2015, 36(10):1441-1458.
[5]
NORI V, LERMA N, GUSTAVSSON J, et al. Forced oscillations in a mixed-compression inlt at mach 3. 5 for pulse enjine system[J]. Journal of Fluids Engineering, 2006, 128(3):494-506.
[6]
TANGIRALA V E. DEAN A J, CHAPIN D M, et al. Pulsed detonation engine processes:experimerts and simulations[J]. Combustion Science Technology, 2004, 176(10):1779-1808.
[7]
李海鹏, 何立明, 陈鑫, 等. 凹面腔内激波聚焦起爆爆震波过程的数值模拟[J]. 推进技术, 2010, 31(1): 87-91.
[8]
荣康, 何立明, 张建邦, 等. 喷口导流环结构对激波聚焦起爆的影响分析[J]. 推进技术, 2012, 33(2): 299-305.
[9]
蔡晓东, 梁剑寒, 林志勇, 等. 基于自适应网格加密的超声速可燃气热射流起爆详细反应数值模拟[J]. 航空动力学报, 2014, 29(10): 2385-2392.
[10]
HAN Xu, ZHOU Jin, LIN Zhiyong. Experimental investigations of detonation initiation by hot jets in super-sonic premixed flows[J]. Chinese Physics: B, 2012, 21(12): 124702.1-124702.5.
[11]
曾昊, 何立明, 章雄伟, 等. 环形射流喷口位置对激波聚焦起爆的影响分析[J]. 推进技术, 2011, 32(3): 437-442.
[12]
何立明, 刁志成, 蒋永健, 等. 连续超声速射流对撞诱导激波聚焦的机理研究[J]. 推进技术, 2016, 37(12): 2394-2400.
[13]
荣康. 环形向心射流诱导激波聚焦与起爆的实验及数值模拟研究[D]. 西安: 空军工程大学, 2011.
[14]
刁志成. 连续超声速射流对撞诱导激波聚焦的机理研究[D]. 西安: 空军工程大学, 2016.
[15]
曾昊. 两级脉冲爆震发动机的实验研究与数值模拟[D]. 西安: 空军工程大学, 2011.
[16]
荣康. 激波聚焦及起爆爆震的实验与数值模拟研究[D]. 西安: 空军工程大学, 2015.
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