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Shock Wave Attenuation in Milli- or Microtubes for Laminar and Turbulent Flow Regime

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30th International Symposium on Shock Waves 2

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Abstract

In an ideal shock tube, the shock wave and the contact surface propagate with constant velocities, and the test time of the hot flow varies linearly along the tube. The hot flow quantities can be easily calculated from the Hugoniot’s relations when the shock Mach number and driven gas conditions are known [1]. But it has been shown that this ideal behavior can be more or less modified function of two main parameters which are the driven gas pressure P 1 and the tube hydraulic diameter D H.

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Author information

Authors and Affiliations

  1. Aix Marseille University, Polytech Marseille, IUSTI/UMR CNRS 6595, 5 rue Enrico Fermi, Marseille, 13013, France

    David E. Zeitoun

Authors
  1. David E. Zeitoun
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Correspondence to David E. Zeitoun .

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Editors and Affiliations

  1. Department of Mechanical Engineering, Ben-Gurion University of the Negev, Beer Sheva, Israel

    Gabi Ben-Dor

  2. Department of Mechanical Engineering, Ben-Gurion University of the Negev, Beer Sheva, Israel

    Oren Sadot

  3. Department of Mechanical Engineering, Ben-Gurion University of the Negev, Beer Sheva, Israel

    Ozer Igra

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Zeitoun, D.E. (2017). Shock Wave Attenuation in Milli- or Microtubes for Laminar and Turbulent Flow Regime. In: Ben-Dor, G., Sadot, O., Igra, O. (eds) 30th International Symposium on Shock Waves 2. Springer, Cham. https://doi.org/10.1007/978-3-319-44866-4_38

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  • DOI: https://doi.org/10.1007/978-3-319-44866-4_38

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  • Publisher Name: Springer, Cham

  • Print ISBN: 978-3-319-44864-0

  • Online ISBN: 978-3-319-44866-4

  • eBook Packages: EngineeringEngineering (R0)

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