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Flow Phenomena in Microscale Shock Tubes

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28th International Symposium on Shock Waves

Introduction

Recent experiments on small shock tubes, at normal or reduced pressure, have revealed interesting phenomena. For example, Brouillette [1], using pressure instrumentation, has examined the operation of a 5.3 mm shock tube at initial pressures down to 1 mBar for diaphragm pressure ratios up to 105 and found a decrease in shock strength with decreasing scaling parameter ReD/L for a given diaphragm pressure ratio. Garen et al. [2], with an atmospheric 1 mm shock tube that used a quick opening valve instead of diaphragm, reached the same conclusions using laser differential interferometry observations.

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References

  1. Brouillette, M.: Shock waves at microscales. Shock Waves 13, 3–12 (2003)

    Article  Google Scholar 

  2. Garen, W., Meyerer, B., Udagawa, S., Maeno, K.: Shock waves in mini-tubes: influence of the scaling parameter S. In: Hanneman, K., Seiler, F. (eds.) Proceedings of 26th International Symposium on Shock Waves, pp. 1473–1478. Springer, Heidelberg (2009)

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  3. Mirshekari, G., Brouillette, M.: One-dimensional model for microscale shock tube flow. Shock Waves 19, 25–38 (2009)

    Article  Google Scholar 

  4. Parisse, J.D., Giordano, J., Perrier, P., Burtschell, Y., Graur, I.A.: Numerical investigation of micro shock waves generation. Microfluid Nanofluid 6, 699–700 (2009)

    Article  Google Scholar 

  5. Mirshekari, G., Brouillette, M.: Shock waves at microscale. In: 27th International Symposium on Shock Waves, St. Petersburg (July 2009)

    Google Scholar 

  6. Laporte, O.: On the interaction of shock with a constriction, Los Alamos Scientific Laboratory Technical Report No. LA-1740 (1954)

    Google Scholar 

  7. Quirk, J.J.: Amrita – A computational facility (for CFD modeling). In: VKI 29th CFD Lecture Series (1998)

    Google Scholar 

  8. Burtschell, Y., Cardoso, M., Zeitoun, D.E.: Numerical analysis of the reducing driver gas contamination in impulse shock tunnels. AIAA J. 39(12), 2357–2365 (2001)

    Article  Google Scholar 

  9. Mirels, H.: Correlation Formulas for Laminar Shock Tube Boundary Layer. Phys. Fluids 9, 1265–1272 (1966)

    Article  Google Scholar 

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Brouillette, M., Giordano, G., Mirshekari, G., Hébert, C., Parisse, J.D., Perrier, P. (2012). Flow Phenomena in Microscale Shock Tubes. In: Kontis, K. (eds) 28th International Symposium on Shock Waves. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-25688-2_36

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  • DOI: https://doi.org/10.1007/978-3-642-25688-2_36

  • Publisher Name: Springer, Berlin, Heidelberg

  • Print ISBN: 978-3-642-25687-5

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