A Novel Method to Minimize Secondary Loading in a Closed-End Shock Tube

被引:2
作者
Kaviarasu, K. [1 ]
Sundar, S. Shyam [1 ]
Alagappan, P. [1 ]
机构
[1] Indian Inst Technol Madras, Dept Civil Engn, Chennai 600036, Tamil Nadu, India
关键词
Shock wave; Shock tube; Blastwave secondary loading; Reflection wave eliminator;
D O I
10.1007/s40870-023-00384-9
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
The development of shock tubes and understanding of shock wave propagation and its interaction with a model is of significant interest in various domains. In this context, shock tubes effectively recreate the field explosion in controlled laboratory conditions and ensure safety, low cost and repeatability. The blast wave simulators (BWS) are operated in a reflective (for barrier wall, blast absorbent material, etc.) and diffractive (for biofidelic head and torso, In-vivo, etc.) mode. The side wall reflections in refractive mode and end wall reflections from the model in reflective mode shock tube cause secondary loading to the model. In this study, a reflection wave eliminator (RWE) with a flap assembly was developed to minimize secondary loading in closed-end shock tubes, and its performances are discussed. As the first cycle of shock wave crosses the RWE, it will open the flap assembly and helps in minimizing the successive cycles of shock waves. The effect of RWE location and the number of flap openings on shock wave parameters, such as positive peak overpressure and impulse, for the case of two different shock tubes length, such as 3.3 m and 5.3 m, has been studied. It was observed that the peak overpressure reduction in the secondary shock wave because of single flap RWE at the model location is 71.31% and 88.12% for 3.3 m and 5.3 m long shock tubes, respectively. The secondary loading of the model in closed-end shock tubes can be significantly reduced by tuning the standard shock tube using the RWE proposed in this study.
引用
收藏
页码:286 / 299
页数:14
相关论文
共 31 条
  • [1] Anderson J.D., 1990, Modern Compressible Flow with Historical Perspective of Aeronautical and Aerospace Engineering
  • [2] ASCE, 2011, BLAST PROT BUILD
  • [3] Experimental investigation of the stress wave propagation inside a granular column impacted by a shock wave
    Belov, E.
    Blachman, M.
    Britan, A.
    Sadot, O.
    Ben-Dor, G.
    [J]. SHOCK WAVES, 2015, 25 (06) : 675 - 681
  • [4] The pathobiology of blast injuries and blast-induced neurotrauma as identified using a new experimental model of injury in mice
    Cernak, Ibolja
    Merkle, Andrew C.
    Koliatsos, Vassilis E.
    Bilik, Justin M.
    Luong, Quang T.
    Mahota, Theresa M.
    Xu, Leyan
    Slack, Nicole
    Windle, David
    Ahmed, Farid A.
    [J]. NEUROBIOLOGY OF DISEASE, 2011, 41 (02) : 538 - 551
  • [5] Evolution of blast wave profiles in simulated air blasts: experiment and computational modeling
    Chandra, N.
    Ganpule, S.
    Kleinschmit, N. N.
    Feng, R.
    Holmberg, A. D.
    Sundaramurthy, A.
    Selvan, V.
    Alai, A.
    [J]. SHOCK WAVES, 2012, 22 (05) : 403 - 415
  • [6] A New Shock Tube Facility for Tunnel Safety
    Colombo, M.
    di Prisco, M.
    Martinelli, P.
    [J]. EXPERIMENTAL MECHANICS, 2011, 51 (07) : 1143 - 1154
  • [7] Commerford GL., 1970, EXPTL MECHANICS, V10, P120, DOI 10.1007/BF02325116
  • [8] Towards a shock tube method for the dynamic calibration of pressure sensors
    Downes, Stephen
    Knott, Andy
    Robinson, Ian
    [J]. PHILOSOPHICAL TRANSACTIONS OF THE ROYAL SOCIETY A-MATHEMATICAL PHYSICAL AND ENGINEERING SCIENCES, 2014, 372 (2023):
  • [9] 110 years of experiments on shock tubes
    Fomin N.A.
    [J]. Journal of Engineering Physics and Thermophysics, 2010, 83 (06) : 1118 - 1135
  • [10] THE DIFFRACTION OF SOUND PULSES .1. DIFFRACTION BY A SEMI-INFINITE PLANE
    FRIEDLANDER, FG
    [J]. PROCEEDINGS OF THE ROYAL SOCIETY OF LONDON SERIES A-MATHEMATICAL AND PHYSICAL SCIENCES, 1946, 186 (1006): : 322 - 344