Volume 32 Issue 10
Oct.  2017
Turn off MathJax
Article Contents
Impact of depth of deflector on shock wave focusing processes in wedgeshaped cavity[J]. Journal of Aerospace Power, 2017, 32(10): 2321-2329. doi: 10.13224/j.cnki.jasp.2017.10.003
Citation: Impact of depth of deflector on shock wave focusing processes in wedgeshaped cavity[J]. Journal of Aerospace Power, 2017, 32(10): 2321-2329. doi: 10.13224/j.cnki.jasp.2017.10.003

Impact of depth of deflector on shock wave focusing processes in wedgeshaped cavity

doi: 10.13224/j.cnki.jasp.2017.10.003
  • Received Date: 2016-01-27
  • Publish Date: 2017-10-28
  • In order to obtain the influence of the depth of deflector on the process of shock wave focusing in a wedgeshaped cavity, tests and numerical simulation studies were carried out to investigate shock focusing on a test section where the depth of deflector was 0, 5, 10,15mm. CCD(charge coupled device) camera was used to obtain the schlieren photos of the flow field. Pressure sensors were used to record the pressure histories. The numerical simulation of the process was carried out by using the numerical method with high accuracy. The shock wave focusing processes of different deflectors were compared. Result showed that, with the increase of depth, the time between leading shock focusing and compressional wave focusing decreased. Because of that, the strength of shock wave focusing and the peak of pressure in bottom of cavity increased. The depth of deflector can determine the forming time of secondary shock and its degree of development, and then influence the disorder degree of the flow field during the shock wave focusing process.

     

  • loading
  • [1]
    LEVIN V A,NECHAEV J N,TARASOV A I.A new approach to organizing operation cycles in pulse detonation engines[R].Moscow:HighSpeed Deflagration and Detonation,2001.
    [2]
    严传俊,刘军,范玮,等.脉冲爆震发动机工作原理与循环分析[J].推进技术,1996,17(3):56-63. YAN Chuanjun,LIU Jun,FAN Wei,et al.Operating principle and cycle analysis of pulse detonation engine[J].Journal of Propulsion Technology,1996,17(3):56-63.(in Chinese)
    [3]
    严传俊,范玮,郑龙席,等.脉冲爆震发动机原理及关键技术[M].西安:西北工业大学出版社,2005.
    [4]
    ROY G,FROLOV S,BORISOV A,et al.Pulse detonation propulsion:challenges,current status,and future perspective[J].Progress in Energy and Combustion Science,2004,30(6):545-672.
    [5]
    LEVIN V A,AFONINA N E,GROMOV V G.The dynamics of combustion products flow in ring nozzle with a halfclosed cavity[J].Combustion Science and Technology,2010,182(11/12):1564-1579.
    [6]
    LEYVA I A,TANGIRALA V,DEAN A J.Investigation of unsteady flow field in a 2stage PDE resonator[R].Reno:The 41st Aerospace Sciences Meeting and Exhibit,2003.
    [7]
    MCMANUS K R,DEAN A J.Experimental evaluation of a twostage pulse detonation combustor[R].Tucson,Arizona:The 41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit,2005.
    [8]
    TAKI S,FUJIWARA T A.Numerical study of detonation resonator[R].Moscow:Application of Detonantion to Propulsion,2004.
    [9]
    周鸿.两步法高频爆震发动机(twostage PDE)机理与特性研究[D].南京:南京航空航天大学,2008. ZHOU Hong.Investigation on the basic theory and characteristic of twostage high frequency pulse detonation engine[D].Nanjing:Nanjing University of Aeronautics and Astronautics,2008.(in Chinese)
    [10]
    姜日红,武晓松,王栋.共振型PDE谐振腔喷嘴匹配关系研究[J].航空动力学报,2009,24(5):1006-1010. JIANG Rihong,WU Xiaosong,WANG Dong.Matching research of resonant PDEs resonator and jet[J].Journal of Aerospace Power,2009,24(5):1006-1010.(in Chinese)
    [11]
    邱彦杰.两级脉冲爆震发动机数值模拟[D].南京:南京理工大学,2011. QIU Yanjie.Simulation study of two stage pulse detonation engine[D].Nanjing:Nanjing University of Science and Technology,2011.(in Chinese)
    [12]
    李海鹏.两级脉冲爆震发动机中激波会聚起爆过程的数值模拟研究[D].西安:空军工程大学.2010. LI Haipeng.Simulation study of shock wave focusing of two stage pulse detonation engine[D].Xian:Air Force Engineering University,2010.(in Chinese)
    [13]
    张强,何立明,陈鑫,等.两级脉冲爆震发动机的理想热力循环和性能分析[J].推进技术,2012,33(4):499-454. ZHANG Qiang,HE Liming,CHEN Xin,et al.Ideal thermodynamic cycle and performance analys of 2stage pulse detonation engine[J].Journal of Propulsion Technology,2012,33(4):499-454.(in Chinese)
    [14]
    张强,陈鑫,何立明,等.矩形喷口欠膨胀超声速射流对撞的实验研究[J].物理学报,2013,62(8):360-365. ZHANG Qiang,CHEN Xin,HE Liming,et al.An experimental study of rectangular underexpanded supersonic jets collision[J].Acta Physica Sinica,2013,62(8):360-365.(in Chinese)
    [15]
    曾昊.两级爆震发动机中的实验与数值模拟[D].西安:空军工程大学,2011. ZENG Hao.Experimental study and numerical simulation of two stage pulse detonation engine[D].Xian:Air Force Engineering University,2011.(in Chinese)
    [16]
    曾昊,何立明,荣康,等.凹面腔内的激波会聚冷态实验[J].航空动力学报,2012,27(12):2655-2659. ZENG Hao,HE Liming,RONG Kang,et al.Experiment on shock wave focus in resonator[J].Journal of Aerospace Power,2012,27(12):2655-2659.(in Chinese)
    [17]
    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. RONG Kang.Experimental study and numerical simulation of shock wave focusing and detonation initiation through annular jet collision[D].Xian:Air Force Engineering University,2011.(in Chinese)
    [18]
    荣康,陈鑫,何立明,等.暂冲式环形射流诱导非定常激波聚焦的机理研究[J].推进技术,2015,36(6):824-831. RONG Kang,CHEN Xin,HE Liming,et al.Investigation on mechanism of unsteady shock waves focus induced by blowdown imploding annular jet[J].Journal of Propulsion Technology,2015,36(6):824-831.(in Chinese)
    [19]
    SHU C W.High order ENO and WENO schemes[M].New York:SpringerVerlag,1999.
    [20]
    BERGER M J,OLIGER J.Adaptive mesh refinement for hyperbolic partial differential equations[J].Journal of Computational Physics,1984,53(3):484-512.
    [21]
    DEITERDING R.Blockstructured adaptive mesh refinementtheory,implementation and application[J].Esaim Proceedings,2011,34:97-150.
    [22]
    LAW C,MURITALA A O,SKEWS B W.Unsteady flow with separation behind a shock wave diffracting over curved walls[J].Shock Waves,2014,24:283-294.
  • 加载中

Catalog

    通讯作者: 陈斌, bchen63@163.com
    • 1. 

      沈阳化工大学材料科学与工程学院 沈阳 110142

    1. 本站搜索
    2. 百度学术搜索
    3. 万方数据库搜索
    4. CNKI搜索

    Article Metrics

    Article views (991) PDF downloads(493) Cited by()
    Proportional views
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return