Skip to main content
Log in

A chemical shock tube driven by detonation

  • Original Article
  • Published:
Shock Waves Aims and scope Submit manuscript

Abstract

A chemical shock tube driven by a detonation driver is described in the present paper. This shock tube can produce a single controlled high-temperature pulse for studies of gas-phase reaction kinetics, but the difficulty associated with the timing for the rupture of diaphragms in the conventional chemical shock tube is overcome, because the detonation wave in the driver section can be predicted correctly and shows a good repeatability. In addition, this shock tube is capable of providing higher temperature conditions for the test gas than the conventional high-pressure shock tube, owing to the inherently high-driving capability of the detonation driver. The feasibility of this shock tube is examined by numerical simulations and preliminary experiments.

This is a preview of subscription content, log in via an institution to check access.

Access this article

Price excludes VAT (USA)
Tax calculation will be finalised during checkout.

Instant access to the full article PDF.

Similar content being viewed by others

References

  1. Greene E.F., Taylor R.L., Patterson W.L. Jr: Pyrolysis of simple hydrocarbons in shock waves. J. Phys. Chem. 62, 238–243 (1958)

    Article  Google Scholar 

  2. Marshall R., Davidson N.: Photoelectric observation of the rate of recombination of iodine atoms. J. Chem. Phys. 21, 659–664 (1953)

    Article  Google Scholar 

  3. Glick, H.S., Squire, W., Hertzberg, A.: A new shock tube technique for the study of high temperature gas phase reactions. In: The Fifth (International) Symposium on Combustion, Pittsburg, Pennsylvania, August 30–September 3, 1954, pp. 393–402. Reinhold, New York (1955)

  4. Lifshitz A., Bauer S.H., Resler E.L.: Studies with single-pulse shock tube. I. The cis-trans isomerization of betene-2. J. Chem. Phys. 38, 2056–2063 (1963)

    Article  Google Scholar 

  5. Fang B.C., Cui J.P.: Single-pulse tube with a magic hole. Aerodyn. Exp. Meas. Control 4, 58–62 (1990)

    Google Scholar 

  6. Bird, G.A.: A note on combustion driven shock tubes. AGARD Report No. 146 (1957)

  7. Lee B.H.K.: Detonation driven in a shock tube. AIAA J. 5(4), 791–792 (1967)

    Article  Google Scholar 

  8. Yu H.R., Esser B., Lenartz M., Groenig H.: Gaseous detonation driver for a shock tunnel. Shock Waves 2(4), 245–254 (1992)

    Article  Google Scholar 

  9. Erdos, J.I., Bakos, R.J., Rogers, R.C.: Dual mode shock expansion/reflected-shock tunnel. AIAA Paper 97-0560 (1997)

  10. Lu F.K., Wilson D.R., Bakos R.J., Erdos J.I.: Recent advances in detonation techniques for high-enthalpy facilities. AIAA J. 38(9), 1676–1684 (2000)

    Article  Google Scholar 

  11. Fickett W., Davis W.C.: Detonation Theory and Experiment. Dover, Mineola (1979)

    Google Scholar 

  12. Olivier, H., Jiang, Z.L., Yu, H.R.: Detonation-driven shock tubes and tunnels. Advanced hypersonic test facilities. In: Lu, F., Marren, D. (eds.) Progress in Astronautics and Aeronautics, vol. 198, pp. 135–205. AIAA (2002)

  13. Lifshitz, A.: The Single Pulse Shock: Its Odyssey in Chemical Kinetics. In: Jiang, Z. (ed.) Proceedings of the 24th International Symposium on Shock Waves, pp. 57–64, Beijing, July 11–16, 2004 (2004)

  14. Gaydon A.G., Hurle I.R.: The Shock Tube in High-Temperature Chemical Physics. Chapman and Hall, London (1963)

    Google Scholar 

  15. Reynolds, W.C.: The Element Potential Method for Chemical Equilibrium Analysis: Implementation in the Interactive Program STANJAN, Version 3. Mechanical Engineering Department, Stanford University (1986)

  16. Li J.P., Feng H., Jiang Z.L.: Numerical computation on the tailored shock mach numbers for a hydrogen-oxygen detonation shock tube. Acta Aerodyn. Sin. 26(3), 291–296 (2008)

    Google Scholar 

  17. Li J.P., Jiang Z.L., Chen H.: Numerical study on backward- forward double detonation driver for high-enthalpy shock tubes. Chin. J. Theor. Appl. Mech. 39(3), 343–349 (2007)

    MathSciNet  Google Scholar 

  18. Jiang Z.L., Takayama K., Chen Y.S.: Dispersion conditions for non-oscillatory shock capturing schemes and its applications. Comput. Fluid Dyn. J. 4(2), 137–150 (1995)

    Article  Google Scholar 

  19. Sichel M., Tonello N.A., Oran E.S., Jones D.A.: A two-step kinetics model for numerical simulation of explosion and detonation in H2–O2 mixtures. Proc. R. Soc. Lond. A 458, 49–82 (2002)

    Article  MATH  Google Scholar 

  20. Zhang X.Y., Yu H.R.: Turbulent Jet Initiation of Oxy-hydrogen Direct Detonation. Aerodyn. Exp. Measur. Control 10(2), 63–68 (1996)

    MathSciNet  Google Scholar 

  21. Hertzberg A., Glick H.S.: Kinetics studies in a single-pulse shock tube. In: Ferri, A. (ed) Fundamental Data Obtained from Shock-Tube Experiments, pp. 161–182. Pergamon Press, London (1961)

    Google Scholar 

Download references

Author information

Authors and Affiliations

Authors

Corresponding author

Correspondence to J. Li.

Additional information

Communicated by H. Olivier.

Rights and permissions

Reprints and permissions

About this article

Cite this article

Li, J., Chen, H. & Yu, H. A chemical shock tube driven by detonation. Shock Waves 22, 351–362 (2012). https://doi.org/10.1007/s00193-012-0374-y

Download citation

  • Received:

  • Revised:

  • Accepted:

  • Published:

  • Issue Date:

  • DOI: https://doi.org/10.1007/s00193-012-0374-y

Keywords

Navigation