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凹面腔内二维激波会聚特性研究 被引量:6

Investigation on two-dimensional shock wave focusing
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摘要 为了研究凹面腔内二维激波会聚的特性,设计、建立了二维激波会聚冷态实验系统,进行了二维激波会聚冷态实验,结果表明:当射流入口宽度增大时,相同射流入射压力下,喷入凹面腔内的射流强度增大,导致凹面腔内的激波会聚强度增强,从而压力脉动幅值增大,频率也随之增大。数值模拟了二维冷态激波会聚过程,从模拟结果中的压力和频率上看,模拟结果与实验结果基本上是吻合的。 In order to study of two-dimensional investigate two-dimensional shock wave focusing characteristics, an experimental shock wave focusing was carried out on a two-dimensional shock wave focusing device, and a relevant numerical simulation was also done. Effects of the jet width and pressure on airflow oscillation frequency were acquired. An increased jet intensity led to an increased shock wave focusing inten- sity, and thus an increased pressure fluctuation and also an increased oscillation frequency. The simulation results were consistent with the experimental results.
出处 《空气动力学学报》 CSCD 北大核心 2013年第3期316-320,共5页 Acta Aerodynamica Sinica
关键词 两级脉冲爆震发动机 爆震波 激波会聚 激波 two-stage pulse detonation engine detonation wave shock wave focus shock wave
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  • 1Lu F K, Meyers J M, Wilson D R. Experimental study of a pulse detonation rocket with shchelkin spiral [ A ]. Proceedings of the 24^th International Symposium on Shock Waves ( Volume 2 )[C]. Beijing : Tsinghua University Press and Spring-Verlag Berlin Heidelberg, 2005. 被引量:1
  • 2Roy G D, Frolov S M, Borisov A A, et al. Pulse detonation propulsion: challenges, current status, and future perspective [ J]. Progress in Energy and Combustion Science, 2004,30 ( 2 ). 被引量:1
  • 3Tangirala V E, Dean A J, Chapin D M. Pulse detonation engine progress: experiments and simulations [ J]. Combust Sci. Tech. ,200d, 76(6). 被引量:1
  • 4Medvedev S P, Khomik S V, Gelfand B E, et al. Shock tube study of hydrogen-Air detonation induced by shock focussing [ A ]. Proceedings of the International Workshop on Shock Wave Focusing Phenomena in Combustible Mixtures: Ignition and Transition to Detonation of Reactive Media Under Geometrical Constraints [ C ]. Aachen, Germany, 1998. 被引量:1
  • 5Levin V A, Nechaev J N, Tarasov A I. A new approach to organizing operation cycles in pulse detonation engines [ C ]. Moscow : High-Speed Deflagration and Detonation: Fundamentals and Control, 2001. 被引量:1
  • 6Ivett A L, Venkat T, Anthony J D. Investigation of unsteady flow field in a 2-Stage PDE resonator [ R]. AIAA 2003-0715. 被引量:1
  • 7Keith R M, Anthony J D. Experimental evaluation of a two-stage pulse detonation combustor [ R ]. AIAA 2005- 3773. 被引量:1
  • 8KONNOV A A. Refinement of the kinetic mechanism of hydrogen combustion [ J ]. Khimicheskaya Fizika, 2004, 23 (8). 被引量:1
  • 9KONNOV A A. Remaining uncertainties in the kinetic mechanism of hydrogen combustion [J]. Combust Flame, 2008,152(4). 被引量:1
  • 10Guderley G. Starke kugelige und zylindrische verdiehtungssthi 3e in der niihe des kugelmittel-punktes bzw[J]. der Zylinderachse Luftfahrtforschung, 1942, 19 (9) 302-312. 被引量:1

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